M PD
A330
MAINTENANCE PLANNING
DOCUMENT
MPD
ENV
The content of this document is the property of Airbus.
It is supplied in confidence and commercial security on its contents must be
maintained.
It must not be used for any purpose other than that for which it is supplied, nor
may information contained in it be disclosed to unauthorized persons. It must not
be reproduced in whole or in part without permission in writing from the owners of
the copyright.
Requests for reproduction of any data in this document and the media authorized
for it must be addressed to Airbus.
© AIRBUS S.A.S. 2005. All rights reserved.
Customer Services Directorate
Maintenance Planning and Services
31707 Blagnac Cedex
FRANCE
REVISION 26, Jul 01/21
ISSUE Jul 01/21
MAINTENANCE PLANNING DOCUMENT
1- M ANU
ALFRONTM ATTER
TRANSMITTAL LETTER REVISION 26, JUL 01/21
1. INSTRUCTIONS
This issue replaces A330 MPD Revision 25, MAR 01/20.
ISSUE: JUL 01/21
TRANSMITTAL LETTER REVISION 26, JUL 01/21
Page 1
MAINTENANCE PLANNING DOCUMENT
2. REASON FOR REVISION
This revision of the MPD was established to reflect changes from:
•
•
•
•
•
•
•
•
•
•
•
•
•
A330 MRBR (Maintenance Review Board Report) Revision 20.
A330 MRBR (Maintenance Review Board Report) Temporary Revision 19.2 and Temporary Revision
19.3.
ALS Part 2 Damage Tolerant Airworthiness Limitation Items (DT-ALI), Revision 04.
ALS Part 3 Certification Maintenance Requirements (CMR), Revision 07.
ALS Part 4 System Equipment Maintenance Requirements (SEMR), Revision 08.
ALS Part 5 Fuel Airworthiness Limitations (FAL), Revision 04.
ETOPS, Configuration, Maintenance, Procedure (CMP) document Revision 34.
Corrections identified since previous MPD revision.
Updated AMM references.
Task man–hours review.
Task preparation review (including preparation MH).
Task access review (including access MH).
MOD SB review for MPD applicability expressions.
ISSUE: JUL 01/21
TRANSMITTAL LETTER REVISION 26, JUL 01/21
Page 2
MAINTENANCE PLANNING DOCUMENT
3. HIGHLIGHTS OF CHANGES
•
•
•
•
MPD task changes are highlighted and explained in a separate column (Reason/Justification):
• in PDF/Excel format in the “SOC”
• in AirN@v/Planning in the “Highlights”.
Some task notes have been updated in accordance with the MPD Simplification (as mentioned in OIT
999.0121/16 "Simplification of the Maintenance Planning Document).
References to the AirPl@n Simulator and AirPl@n Examples have been removed from this MPD. The
Airpl@n Simulator on Airbusworld is not anymore updated.
Appendix 7 “LANDING GEAR OVERHAUL PROCEDURES” replaced.
ISSUE: JUL 01/21
TRANSMITTAL LETTER REVISION 26, JUL 01/21
Page 3
MAINTENANCE PLANNING DOCUMENT
4. IMPORTANT NOTES
•
•
•
•
•
Information from new or revised source documents, which have been received after closure of MPD
authoring will be considered with next MPD Revision.
The Airn@v Planning version of this MPD contains only non range sensitive requirements together
with the FH-optimized limits
For MPD revision information go to AirbusWorld/Maintenance & Engineering/ Prepare Maintenance/
Prepare maintenance program/ select the relevant aircraft program under “Consult Airbus
maintenance requirements“ and thereafter select “Revision Information“ enlisted under “MPD
Information“.
For some MPD tasks, an AMM procedure was not available at the time of the MPD compilation.
NOTE: Please contact the AMM department via TechRequest (domain: Technical Manuals), if you
urgently need an AMM procedure.
The operator should be aware of manufacturer and vendor recommendations and/or requirements
published through Inspection Service Bulletin (ISB), In-Service Information (ISI), Service Information
Letter (SIL), All Operators Letter (AOL), Alert Operators Transmission (AOT) and similar documents
dealing with scheduled maintenance. These are no longer reflected in the MPD and it is thus the
operator’s responsibility to review these and determine whether or not to include them in their locally
approved programs.
ISSUE: JUL 01/21
TRANSMITTAL LETTER REVISION 26, JUL 01/21
Page 4
MAINTENANCE PLANNING DOCUMENT
SUMMARY OF CHANGES
MPD
SEC
TASK NUMBER
2-20
200003-01-1
2-20
2-21
200151-09-1
212800-02-4
2-21
215100-01-1
2-21
215200-01-1
2-22
221000-01-2
2-23
237100-01-1
2-23
237100-02-1
2-23
237135-01-1
2-23
237135-02-1
2-24
242100-23-2
2-24
242100-25-1
2-24
242100-27-1
M
V DESCRIPTION
T
R ZONE "193" REMOVED
IN ZONE "193" MEN: "1" REMOVED
IN ZONE "193" TASK MH: "0.40" REMOVED
IN ZONE "193" ACCESS MH: "1.60" REMOVED
IN ZONE "193" ACCESS: "193AB" REMOVED
ZONE "191" ADDED
IN ZONE "191" MEN: "1" ADDED
IN ZONE "191" TASK MH: "0.40" ADDED
IN ZONE "191" ACCESS MH: "3.70" ADDED
IN ZONE "191" ACCESS: "191FB; 191KB" ADDED
R TASK CODE CHANGED FROM: "GVI", TO: "RST"
R IN SOURCE: "CMR**" ADDED
IN SOURCEREFERENCE: "(CMR**) CMR 21280000002-1-C" ADDED
100% INTERVAL CHANGED FROM: "3200 FH", TO:
"2500 FH"
R APPLICABILITY CHANGED FROM: "POST 50213
(21-3080)", TO: "IF P/N 964F0000-XX INSTALLED"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-800 OR A330-900", TO: "ALL"
R 100% INTERVAL CHANGED FROM: "42 MO", TO:
"72 MO"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
R APPLICABILITY CHANGED FROM: "ETOPS PW PRE
43285 (24-3008) OR ETOPS RR PRE 43286 (243008) OR ETOPS GE PRE 43286 (24-3008)", TO:
"ETOPS RR PRE 43286 (24-3008)"
R APPLICABILITY CHANGED FROM: "A330-800 OR
A330-900", TO: "A330-900 PRE 209109"
N NEW TASK ADDED
2-24
242100-28-1
N
ISSUE: JUL 01/21
NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
TASK CODE REVIEW
CMR REV.07
MRBR REV.20
MRBR REV.20
CMP REV.34
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
TASK SPLIT TO 24210027-1 AND 242100-28-1
MRBR REV.20
TASK SPLIT FROM
242100-23-2
TASK SPLIT FROM
242100-23-2
Page 1
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-24
242400-03-2
2-24
243500-03-1
2-25
2-25
2-25
2-25
252100-09-1
252100-10-1
252100-11-1
252344-01-1
2-25
252344-02-1
2-25
2-25
252344-03-1
253000-01-1
2-25
255100-01-1
2-25
255200-03-1
2-25
256200-08-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R 100% INTERVAL CHANGED FROM: "42 MO", TO:
"48 MO"
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"1000 FH"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-800 OR A330-900 OR A330200F POST 58673 (25-3625)", TO: "A330-200 OR
A330-300 OR A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-800 OR A330-900 OR A330200F POST 58673 (25-3625)", TO: "A330-200 OR
A330-300 OR A330-800 OR A330-900"
N NEW TASK ADDED
R TASK NOTE "INTERVAL: OPERATORS ARE ADVISED
TO OPTIMISE THE INTERVAL OF THIS TASK
ACCORDING TO THEIR OPERATING
ENVIRONMENT AND EXPERIENCE. THIS MAY
RESULT IN A LESS OR MORE FREQUENT INTERVAL"
ADDED
100% INTERVAL CHANGED FROM: "1400 FH", TO:
"1400 FH NOTE"
R DESCRIPTION CHANGED FROM: "UNITS", TO:
"UNITS."
TASK NOTE CHANGED FROM: "11.", TO: "CREW
REST ROOM (UNDERFLOOR) AND/OR ACTS NOT
TO BE REMOVED IF INSTALLED"
R DESCRIPTION "(NOTE 11)." REMOVED
TASK NOTE "CREW REST ROOM (UNDERFLOOR)
AND/OR ACTS NOT TO BE REMOVED IF
INSTALLED" ADDED
R TASK NOTE CHANGED FROM: "INTERVAL:
INTERVAL TO BE", TO: "INTERVAL: FOR INTERVAL
SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3 INTERVAL TO BE"
100% INTERVAL CHANGED FROM: "180 MO
NOTE", TO: "CE NOTE"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
CMP REV.34
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
NOTE REVIEW
NOTE REVIEW
MRBR REV.20
Page 2
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-25
256241-02-1
2-25
256532-03-1
2-25
2-25
2-25
256532-04-1
256532-05-1
256535-01-1
2-25
256535-03-1
2-25
256535-04-1
2-25
2-25
2-25
2-26
2-26
256535-05-1
256241-01-1
256532-02-1
261100-01-1
262200-01-3
2-26
262200-03-2
2-26
262200-06-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R TASK NOTE CHANGED FROM: "INTERVAL:
INTERVAL TO BE", TO: "INTERVAL: FOR INTERVAL
SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3 INTERVAL TO BE"
IN SOURCE: "MRB 6,8" ADDED AND "MRB 8"
REMOVED
IN SOURCEREFERENCE: "(FEC 6,8) MRB MSI
25.62.00/02" ADDED AND "(FEC 8) MRB MSI
25.62.00/02" REMOVED
100% INTERVAL CHANGED FROM: "36 MO NOTE",
TO: "CE NOTE"
R APPLICABILITY CHANGED FROM: "SURVIVAL ELT
INSTALLED", TO: "IF SURVIVAL ELT FROM
HONEYWELL 07217 INSTALLED OR IF SURVIVAL
ELT FROM THALES FAU27 INSTALLED OR IF
SURVIVAL ELT FROM ELTA FORMER CEIS 649E2
INSTALLED OR IF SURVIVAL ELT FROM ELTA F6614
INSTALLED"
DESCRIPTION CHANGED FROM: "TRANSMITTER
(ELT(S)) FOR IN SHOP BATTERY REPLACEMENT.",
TO: "TRANSMITTER FOR IN SHOP BATTERY
REPLACEMENT AND OPERATIONAL CHECK OF:
WATER SWITCH GPS FUNCTIONALITY 406 MHZ
DISTRESS SIGNAL TRANSMISSION."
TASK CODE CHANGED FROM: "DIS", TO: "RST"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "AUTOMATIC
FIXED ELT INSTALLED", TO: "PRE 208191"
R APPLICABILITY CHANGED FROM: "AUTOMATIC
FIXED ELT INSTALLED", TO: "PRE 208191"
R APPLICABILITY CHANGED FROM: "AUTOMATIC
FIXED ELT INSTALLED", TO: "PRE 208191"
N NEW TASK ADDED
D TASK DELETED
D TASK DELETED
N NEW TASK ADDED
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"1000 FH"
R 100% INTERVAL CHANGED FROM: "42 MO", TO:
"48 MO"
R 100% INTERVAL CHANGED FROM: "42 MO", TO:
"48 MO"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
CMP REV.34
CMP REV.34
CMP REV.34
Page 3
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-26
262200-07-3
2-26
262400-13-1
2-26
262400-14-1
2-27
272100-05-1
2-27
2-27
272100-21-1
272600-05-4
M
V DESCRIPTION
T
R 100% INTERVAL CHANGED FROM: "36 MO OR
8000 FH", TO: "48 MO OR 8000 FH"
R IN REFERENCE(S): "AMT 262400-920-801" ADDED
AND "AMT 262400-280-802" REMOVED
R IN REFERENCE(S): "AMT 262400-920-802" ADDED
AND "AMT 262400-280-806" REMOVED
R 100% INTERVAL CHANGED FROM: "20 MO", TO:
"24 MO"
N NEW TASK ADDED
N NEW TASK ADDED
2-27
274000-19-1
R
2-27
2-27
274000-20-1
274100-01-1
N
R
2-27
274400-16-1
R
ISSUE: JUL 01/21
APPLICABILITY CHANGED FROM: "POST 206264",
TO: "POST 206264 (27-3234)"
NEW TASK ADDED
DESCRIPTION CHANGED FROM: "CHAINS.", TO:
"CHAINS (FWD AND AFT SECTIONS) AND CABLES
(AFT SECTION)."
TASK NOTE CHANGED FROM: "OF 12000 FC", TO:
"OF 8500 FC"
100% THRESHOLD CHANGED FROM: "12000 FC
NOTE", TO: "8500 FC NOTE"
100% INTERVAL CHANGED FROM: "12000 FC", TO:
"8500 FC"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
CMP REV.34
AMM REFERENCE
REVIEW
AMM REFERENCE
REVIEW
MRBR REV.20
MRBR REV.20
TASK CREATED TO
COVER MRBR
REQUIREMENT
MOD SB REVIEW
MRBR REV.20
MRBR REV.20
SEMR REV.08
Page 4
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-27
274400-16-2
2-27
2-27
274400-16-3
275000-02-1
2-27
275000-15-1
2-27
275000-16-1
2-27
275100-01-1
2-27
275400-01-1
2-27
275400-04-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "IF P/N 47172530 INSTALLED", TO: "IF P/N 47172-500
INSTALLED OR IF P/N 47172-510 INSTALLED OR IF
P/N 47172-520 INSTALLED OR IF P/N 47172-530
INSTALLED"
TASK NOTE CHANGED FROM: "THE THRESHOLD
OF 12000 FC IS THE TIME SINCE NEW FOR THSA
ORIGINALLY MANUFACTURED AS PNR 47172-530
OR THE TIME SINCE RETROFIT INTO PNR 47172530 OR THE TIME SINCE NEW FOR SPECIFIC THSA
PNR 47172-530 SNR 503, WHICH WAS
RETROFITTED INTO PNR 47172- 530 WITHOUT
NBB DISKS REPLACEMENT.", TO: "FOR THSA PNRS
47172-500, 47172-510 AND 47172-520
THRESHOLD OF 8500 FC IS THE TIME SINCE NEW
FOR THSA PNR 47172-530 THE THRESHOLD OF
8500 FC IS THE TIME SINCE NEW FOR THSA
ORIGINALLY MANUFACTURED AS PNR 47172-530
OR THE TIME SINCE RETROFIT INTO PNR 47172530 OR THE TIME SINCE NEW FOR SPECIFIC THSA
PNR 47172-530 SNR 503, WHICH WAS
RETROFITTED INTO PNR 47172-530 WITHOUT
NBB DISKS REPLACEMENT"
100% THRESHOLD CHANGED FROM: "12000 FC
NOTE", TO: "8500 FC NOTE"
100% INTERVAL CHANGED FROM: "12000 FC", TO:
"8500 FC"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
IN REFERENCE(S): "AMT 275400-220-805" ADDED
AND "AMT 275400-200-805" REMOVED
R ZONE "630" ADDED
IN ZONE "630" MEN: "1" ADDED
IN ZONE "630" TASK MH: "TBD" ADDED
R ZONE "630" ADDED
IN ZONE "630" MEN: "1" ADDED
IN ZONE "630" TASK MH: "TBD" ADDED
R 100% INTERVAL CHANGED FROM: "18 MO", TO:
"24 MO"
R 100% INTERVAL CHANGED FROM: "60 MO", TO:
"72 MO"
R 100% INTERVAL CHANGED FROM: "3200 FH", TO:
"1500 FC OR 4000 FH"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
SEMR REV.08
SEMR REV.08
SEMR REV.08
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 5
MAINTENANCE PLANNING DOCUMENT
M
V DESCRIPTION
T
R 100% INTERVAL CHANGED FROM: "60 MO", TO:
"72 MO"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
201497"
IN PREPARATION MH : "0.02" ADDED
IN PREPARATION TASKS: "FLAPS EXTENDED;
MAIN GEAR DOORS" ADDED
ZONE "500;600" REMOVED
IN ZONE "500" MEN: "1" REMOVED
IN ZONE "500" TASK MH: "0.15" REMOVED
IN ZONE "500" ACCESS MH: "0.15" REMOVED
IN ZONE "500" ACCESS: "734" REMOVED
IN ZONE "600" MEN: "1" REMOVED
IN ZONE "600" TASK MH: "0.15" REMOVED
IN ZONE "600" ACCESS MH: "0.15" REMOVED
IN ZONE "600" ACCESS: "744" REMOVED
ZONE "147;148" ADDED
IN ZONE "147" MEN: "1" ADDED
IN ZONE "147" TASK MH: "0.15" ADDED
IN ZONE "148" MEN: "1" ADDED
IN ZONE "148" TASK MH: "0.15" ADDED
N NEW TASK ADDED
R 100% INTERVAL CHANGED FROM: "3200 FH", TO:
"1500 FC OR 4000 FH"
R 100% INTERVAL CHANGED FROM: "18 MO", TO:
"24 MO"
R 100% INTERVAL CHANGED FROM: "60 MO", TO:
"72 MO"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330900"
MPD
SEC
TASK NUMBER
2-27
275400-05-1
2-27
275400-06-1
2-27
2-27
275400-06-2
275400-07-1
2-27
275400-08-1
2-27
275500-01-1
2-27
276400-03-1
2-27
2-27
276400-03-2
278000-01-1
N
R
2-27
278000-02-1
R
ISSUE: JUL 01/21
NEW TASK ADDED
100% INTERVAL CHANGED FROM: "2800 FH", TO:
"1500 FC OR 4000 FH"
IN PREPARATION MH CHANGED FROM: "0.12",
TO: "0.10"
IN PREPARATION TASKS: "FLAPS EXTENDED"
REMOVED
IN PREPARATION MH CHANGED FROM: "0.12",
TO: "0.10"
IN PREPARATION TASKS: "FLAPS EXTENDED"
REMOVED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
TASK SPLIT TO 27640003-2, EASA AD 2020054, FAA AD 2020-1509
CMR REV.07
MRBR REV.20
PREPARATION REVIEW
Page 6
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-27
278000-03-1
2-27
278000-04-1
2-27
2-27
2-27
278000-04-3
278000-04-2
278000-06-1
2-27
2-27
278000-11-1
279000-14-2
2-28
281100-07-1
2-28
281100-09-1
2-28
281800-01-1
2-28
281800-02-1
2-28
281800-03-1
2-28
281800-04-1
2-28
281800-07-1
2-28
281800-08-1
2-28
281800-09-1
2-28
281800-10-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R 100% INTERVAL CHANGED FROM: "18 MO", TO:
"24 MO"
R APPLICABILITY CHANGED FROM: "PRE 41410",
TO: "PRE 201497"
N NEW TASK ADDED
D TASK DELETED
R 100% INTERVAL CHANGED FROM: "18 MO", TO:
"24 MO"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 POST
49144 OR A330-300 POST 49144 OR A330-200F
", TO: "A330-200 POST 49144 OR A330-300 POST
49144 OR A330-200F OR A330-800 OR A330-900"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R APPLICABILITY CHANGED FROM: "A330-200 POST
49520 (21-3096) OR A330-200F PRE 58623 OR
A330-200F POST 200281 OR A330-300 POST
204025 OR A330-800 POST 49520 (21-3096) OR
A330-900", TO: "A330-200 POST 49520 (21-3096)
OR A330-200F PRE 58623 OR A330-200F POST
200281 OR A330-300 POST 204025 OR A330-800
OR A330-900"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
R 100% INTERVAL CHANGED FROM: "8 C", TO: "144
MO"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
APPLICABILITY REVIEW
MRBR REV.20
MRBR REV.20
MRBR REV.20
FAL REV.04
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 7
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-28
281800-12-1
2-28
282200-07-4
2-28
282300-02-1
2-28
282600-04-1
2-28
282700-02-4
2-28
283100-01-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "FAA A330-200
POST 200242 (28-3113) OR FAA A330-200F POST
200242 (28-3113) OR FAA A330-300 POST 200242
(28-3113) OR FAA A330-900", TO: "FAA A330-200
POST 200242 (28-3113) OR FAA A330-200F POST
200242 (28-3113) OR FAA A330-300 POST 200242
(28-3113) OR FAA A330-800 OR FAA A330-900"
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"1000 FH"
R 100% INTERVAL CHANGED FROM: "36 MO", TO:
"48 MO"
R APPLICABILITY CHANGED FROM: "A330-200 POST
49144 OR A330-200 POST 200103 (00-3068) OR
A330-200F PRE 58623 OR A330-200F POST
200281 OR A330-300 POST 204025 OR A330-900",
TO: "A330-200 POST 49144 OR A330-200 POST
200103 (00-3068) OR A330-200F PRE 58623 OR
A330-200F POST 200281 OR A330-300 POST
204025 OR A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 PRE
45649 (28-3056) POST 49144 OR A330-200 PRE
45649 (28-3056) POST 58269 OR A330-200 PRE
45649 (28-3056) POST 200103 (00-3068) OR
A330-200 POST 45649 (28-3056) OR A330-300
PRE 45649 (28-3056) POST 49144 OR A330-300
PRE 45649 (28-3056) POST 58269 OR A330-300
PRE 45649 (28-3056) POST 200103 (00-3068) OR
A330-300 POST 45649 (28-3056) OR A330-200F
OR A330-900", TO: "A330-200 PRE 45649 (283056) POST 49144 OR A330-200 PRE 45649 (283056) POST 58269 OR A330-200 PRE 45649 (283056) POST 200103 (00-3068) OR A330-200 POST
45649 (28-3056) OR A330-300 PRE 45649 (283056) POST 49144 OR A330-300 PRE 45649 (283056) POST 58269 OR A330-300 PRE 45649 (283056) POST 200103 (00-3068) OR A330-300 POST
45649 (28-3056) OR A330-200F OR A330-800 OR
A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 POST
45008 (28-3084) OR A330-200F POST 45008 (283084)", TO: "A330-200 POST 45008 (28-3084) OR
A330-200F POST 45008 (28-3084) OR A330-800
POST 206807"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
FAL REV.04
CMP REV.34
CMP REV.34
CMR REV.07
CMR REV.07
MRBR REV.20
Page 8
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-28
283100-02-1
2-28
283100-03-1
2-29
291000-08-1
2-29
291000-23-1
2-29
291700-01-1
2-29
292000-04-1
2-29
2-31
291000-01-1
313300-01-1
2-31
313300-02-1
2-31
313300-03-1
2-31
313300-05-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 POST
45008 (28-3084) OR A330-200F POST 45008 (283084)", TO: "A330-200 POST 45008 (28-3084) OR
A330-200F POST 45008 (28-3084) OR A330-800
POST 206807"
R APPLICABILITY CHANGED FROM: "A330-200 POST
45008 (28-3084) OR A330-200F POST 45008 (283084)", TO: "A330-200 POST 45008 (28-3084) OR
A330-200F POST 45008 (28-3084) OR A330-800
POST 206807"
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"1000 FH"
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"1000 FH"
R 100% INTERVAL CHANGED FROM: "1600 FH", TO:
"2000 FH"
R TASK NOTE "ETOPS RELEVANT" REMOVED
IN SOURCE: "MRB 8" ADDED AND "MRB 6,8"
REMOVED
IN SOURCEREFERENCE: "(FEC 6) MRB MSI
29.10.00/24" REMOVED
D TASK DELETED
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
DESCRIPTION CHANGED FROM: "DISCARD OF ULB
BATTERY.", TO: "REMOVE ULB FOR IN SHOP ULB
BATTERY DISCARD."
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE
208191"
100% INTERVAL CHANGED FROM: "24 MO", TO:
"36 MO"
R APPLICABILITY CHANGED FROM: "POST 56807
(31-3130) PRE 206186 (31-3234) OR POST 58513
(31-3181), (31-3185) PRE 206186 (31-3234)", TO:
"POST 56807 (31-3130) PRE 206186 (31-3234)
PRE 208191 OR POST 58513 (31-3181), (31-3185)
PRE 206186 (31-3234) PRE 208191"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
INTERVAL REVIEW
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 9
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-31
313300-06-1
2-31
2-31
2-31
2-31
2-31
2-31
2-31
2-32
313400-01-1
313400-02-1
313400-03-1
313400-04-1
313400-05-1
313400-06-1
313400-07-1
321100-01-1
2-32
2-32
321100-01-2
321100-02-1
2-32
321100-24-1
2-32
2-32
321100-24-2
321100-30-1
2-32
2-32
321100-30-2
321100-31-1
2-32
321100-32-1
2-32
2-32
321100-32-2
321100-33-1
2-32
2-32
321100-33-2
322100-02-1
2-32
322100-02-2
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "POST 55048
(31-3109), (31-3167) OR POST 56293 (31-3119),
(31-3142), (31-3184), (31-3193), (31-3215), (313233)", TO: "POST 55048 (31-3109), (31-3167)
PRE 208191 OR POST 56293 (31-3119), (31-3142),
(31-3184), (31-3193), (31-3215), (31-3233) PRE
208191"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
N NEW TASK ADDED
R 100% INTERVAL CHANGED FROM: "10 YE", TO:
"12 YE"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208041 OR A330-900 PRE 208041"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 10
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-32
322100-11-1
2-32
2-32
322100-11-2
322100-12-1
2-32
2-32
2-32
322100-12-2
324000-05-1
325300-01-1
2-33
2-33
334800-01-1
335100-01-1
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208041 OR A330-900 PRE 208041"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208041 OR A330-900 PRE 208041"
N NEW TASK ADDED
N NEW TASK ADDED
R IN REFERENCE(S): "AMT 325300-720-801" ADDED
AND "AMT 325300-710-802" REMOVED
N NEW TASK ADDED
R IN REFERENCE(S): "AMT 335100-710-801" ADDED
2-33
335100-02-1
R
2-33
335100-04-1
R
2-33
2-34
335100-08-1
341300-05-1
N
R
ISSUE: JUL 01/21
TASK NOTE CHANGED FROM: "PLANNING: AS AN
ALTERNATIVE, TASK MAY BE ACCOMPLISHED BY
INSTALLATION OF SERVICEABLE BATTERIES (REF
AMM 335138-400-802-A9) PLANNING: FOR
CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE
PERFORMED WHEN CRR(U) IS NEXT INSTALLED",
TO: "PLANNING: AS AN ALTERNATIVE, TASK MAY
BE ACCOMPLISHED BY INSTALLATION OF
SERVICEABLE BATTERIES FOR CRR(U) USERS ONLY:
CRR(U) PART IS INCLUDED IN THIS TASK. IF CRR(U)
IS NOT FITTED WHEN TASK BECOMES DUE, CRR(U)
PART SHOULD BE PERFORMED WHEN CRR(U) IS
NEXT INSTALLED INTERVAL: FOR INTERVAL
SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3 INTERVAL TO BE MANAGED
AT COMPONENT LEVEL"
100% INTERVAL CHANGED FROM: "6 MO NOTE",
TO: "CE NOTE"
TASK NOTE "INTERVAL: FOR INTERVAL SELECTED
FOR THE VARIOUS PART NUMBERS REFER TO
APPENDIX 3 INTERVAL TO BE MANAGED AT
COMPONENT LEVEL" ADDED
100% INTERVAL CHANGED FROM: "6 MO NOTE",
TO: "CE NOTE"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "POST 53368
(34-3213) OR A330 POST 204436", TO: "POST
53368 (34-3213) OR POST 204436 (31-3242)"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
CMR REV.07
AMM REFERENCE
REVIEW
MRBR REV.20
AMM REFERENCE
REVIEW
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 11
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-34
341300-06-2
2-34
342200-01-1
2-34
342200-03-1
2-35
351000-20-1
2-35
352002-21-1
2-35
352142-01-1
2-35
2-36
352142-01-2
360001-02-1
2-36
360001-03-1
2-36
360002-01-1
2-36
360002-02-1
2-36
361251-01-5
2-36
361251-01-6
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R ZONE "210" REMOVED
IN ZONE "210" MEN: "1" REMOVED
IN ZONE "210" TASK MH: "0.35" REMOVED
ZONE "120" ADDED
IN ZONE "120" MEN: "1" ADDED
IN ZONE "120" TASK MH: "0.35" ADDED
R IN ZONE "130" ACCESS MH CHANGED FROM:
"0.81", TO: "1.11"
IN ZONE "130" ACCESS "132EG" ADDED
R 100% INTERVAL CHANGED FROM: "800 FH", TO:
"2000 FH"
R TASK NOTE "INTERVAL: INTERVAL TO BE
MANAGED AT COMPONENT LEVEL" REMOVED
100% INTERVAL CHANGED FROM: "240 MO
NOTE", TO: "240 MO"
R TASK NOTE "INTERVAL: INTERVAL TO BE
MANAGED AT COMPONENT LEVEL" REMOVED
100% INTERVAL CHANGED FROM: "240 MO
NOTE", TO: "240 MO"
R APPLICABILITY CHANGED FROM: "A330-200 PRE
40257 PRE 52485 OR A330-300 PRE 40257 PRE
56322 OR A330-800 PRE 52485 OR A330-900 PRE
56322", TO: "A330-200 PRE 40257 PRE 52485 OR
A330-300 PRE 40257 PRE 56322 OR A330-900
PRE 56322"
N NEW TASK ADDED
R IN SOURCE: "CMR*" ADDED
IN SOURCEREFERENCE: "(CMR*) CMR 36000100001-1-C" ADDED
R IN REFERENCE(S): "AMT 361200-710-805" ADDED
AND "AMT 361200-710-802" REMOVED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 PRE 208995 OR A330-900 PRE
208995"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 PRE 208995 OR A330-900 PRE
208995"
R APPLICABILITY CHANGED FROM: "A330-800 IF PN
2S7138 INSTALLED OR A330-900 IF PN 2S7138
INSTALLED", TO: "A330-800 OR A330-900"
D TASK DELETED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ZONE REVIEW
ACCESS REVIEW
MRBR REV.20
MRBR REV.20
MRBR REV.20
TASK SPLIT TO 35214201-2
SEMR REV.08
CMR REV.07
AMM REFERENCE
REVIEW
SEMR REV.08
SEMR REV.08
MRBR REV.20
MRBR REV.20
Page 12
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-38
381000-02-1
2-49
493100-01-3
2-49
499100-01-2
2-52
521000-07-1
2-52
2-52
2-52
521000-07-2
521000-13-1
522200-01-1
2-52
522200-09-1
2-52
2-52
522200-09-2
525111-06-1
2-52
527100-04-1
2-56
2-72
561000-02-2
722100-G1-1
2-72
723200-G1-1
2-72
723100-P6-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R TASK NOTE "INTERVAL: OPERATORS ARE ADVISED
TO OPTIMISE THE INTERVAL OF THIS TASK
ACCORDING TO THEIR OPERATING
ENVIRONMENT AND EXPERIENCE. THIS MAY
RESULT IN A LESS OR MORE FREQUENT INTERVAL"
ADDED
100% INTERVAL CHANGED FROM: "3 MO", TO: "3
MO NOTE"
R TASK NOTE CHANGED FROM: "EVERY 1000 AH.
TASK TO BE ACCOMPLISHED AT 150FH AND 400FH
AFTER MAJOR TANK REPAIR. THEREAFTER EVERY
1000AH. ETOPS", TO: "EVERY 1500 AH. TASK TO
BE ACCOMPLISHED AT 150FH AND 400FH AFTER
MAJOR TANK REPAIR. THEREAFTER EVERY
1500AH. ETOPS"
100% INTERVAL CHANGED FROM: "1000 AH
NOTE", TO: "1500 AH NOTE"
R TASK NOTE "TASK ONLY APPLICABLE TO APU
EQUIPPED WITH OIL PUMP PN 3881000-6."
REMOVED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330900"
N NEW TASK ADDED
N NEW TASK ADDED
R DESCRIPTION CHANGED FROM: "OPEN
POSITION.", TO: "OPEN POSITION, AND
ACTUATOR DAMPENING AND FRICTIONLESS
EXTENSION/RETRACTION."
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-800 OR A330-900", TO: "A330200 OR A330-300 OR A330-900"
N NEW TASK ADDED
R DESCRIPTION CHANGED FROM: "SWITCH OVER.",
TO: "SWITCH OVERRIDE."
R IN ZONE "210" TASK MH CHANGED FROM: "0.10",
TO: "0.40"
N NEW TASK ADDED
R 100% INTERVAL CHANGED FROM: "4500 FH", TO:
"5000 FH"
R 100% INTERVAL CHANGED FROM: "2 A", TO:
"2000 FH"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
NOTE REVIEW
CMP REV.34
NOTE REVIEW
TASK SPLIT TO 52100007-2
SEMR REV.08
MRBR REV.20
MRBR REV.20
TASK SPLIT TO 52220009-2
SEMR REV.08
MRBR REV.20
TASK MH REVIEW
MRBR REV.20
INTERVAL REVIEW
CMP REV.34
MRBR REV.20
Page 13
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
2-72
724100-P1-1
2-72
723112-P1-1
M
V DESCRIPTION
T
R IN REFERENCE(S): "AMT 720000-290-832" ADDED
AND "AMT 720000-290-833" REMOVED
D TASK DELETED
2-73
2-78
732000-P1-1
781100-R1-1
N
R
2-78
783100-N1-1
R
2-79
2-79
792000-P6-1
793000-R4-1
N
R
3-32
321107-02-1
R
3-32
3-32
321107-02-2
321125-03-1
N
R
3-32
3-32
321193-02-1
322102-02-1
N
R
3-32
322110-02-2
R
3-32
3-32
322110-02-3
322119-01-2
N
R
3-32
3-52
322119-01-3
521201-01-2
N
R
3-52
521301-01-2
R
ISSUE: JUL 01/21
NEW TASK ADDED
100% INTERVAL CHANGED FROM: "1600 FH", TO:
"2000 FH"
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "TRENT 700
WITH EMCD INSTALLED BUT NOT ACTIVATED
POST SB RB 79-G229 PRE SB RB 79-F524", TO:
"TRENT 700 PRE 56713 IF EMCD INSTALLED"
APPLICABILITY CHANGED FROM: "A330-200 PRE
54500 OR A330-300 PRE 54500", TO: "A330-200
PRE 54500 OR A330-300 PRE 54500 OR A330-800
PRE 54500 OR A330-900 PRE 54500"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208040 OR A330-900 PRE 208040"
NEW TASK ADDED
DESCRIPTION CHANGED FROM: "TUBE INCLUDING
AXLE, EXTERNAL SURFACE, EXCEPT WHERE
COVERED BY DRESSINGS, FITTINGS AND BUSH
FLANGES.", TO: "TUBE, EXTERNAL SURFACE."
IN PREPARATION TASKS: "SLIDING TUBE FULLY
EXTENDED" ADDED AND "NLG SLEEVES; NLG
WHEELS" REMOVED
APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208041 OR A330-900 PRE 208041"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 PRE 208041 OR A330-900 PRE 208041"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
AMM REFERENCE
REVIEW
TASK TRANSFERRED
TO 723100-P6-1
MRBR REV.20
INTERVAL REVIEW
CMR REV.07
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 14
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-52
522201-01-2
3-52
523101-01-2
3-52
523103-02-1
3-52
523104-01-1
3-52
523104-01-3
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-300 OR A330-200F"
IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 523104-01-2"
ADDED
N NEW TASK ADDED
3-52
523105-01-1
R
3-52
523105-01-2
R
3-52
3-52
523105-02-1
523201-01-2
N
R
3-52
523202-01-2
R
3-52
523203-02-1
R
3-52
523204-01-1
R
3-52
523204-01-3
N
ISSUE: JUL 01/21
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
APPLICABILITY CHANGED FROM: "A330-200F", TO:
"A330-200F OR A330-800 OR A330-900"
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-300 OR A330-200F"
IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 523204-01-2"
ADDED
NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20, ALI
REV.04, TASK SPLIT TO
523104-01-3
MRBR REV.20, TASK
SPLIT FROM 52310401-1
MRBR REV.20
ALI REV.04
MRBR REV.20
MRBR REV.20
APPLICABILITY REVIEW
MRBR REV.20
MRBR REV.20, ALI
REV.04, TASK SPLIT TO
523204-01-3
MRBR REV.20, TASK
SPLIT FROM 52320401-1
Page 15
MAINTENANCE PLANNING DOCUMENT
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-300 OR A330-200F"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
R APPLICABILITY CHANGED FROM: "GROUP 32E OR
GROUP 32F OR GROUP 33E", TO: "GROUP 32E OR
GROUP 32F OR GROUP 33E OR GROUP 38E OR
GROUP 39E"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300"
MPD
SEC
TASK NUMBER
3-52
523205-01-1
3-52
523205-01-2
3-52
3-52
523205-02-1
523212-01-1
3-52
523212-01-2
3-52
523301-01-3
3-52
523303-01-2
3-52
524101-01-2
3-52
3-52
3-52
524101-01-3
524103-01-4
528104-01-2
3-52
528104-01-4
N
NEW TASK ADDED
3-52
528203-01-3
R
3-53
3-53
531110-02-4
531111-01-3
N
R
IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 528203-01-3"
ADDED
100% THRESHOLD CHANGED FROM: "6 YE", TO: "6
YE OR 9600 FC"
100% INTERVAL CHANGED FROM: "6 YE", TO: "6
YE OR 9600 FC"
NEW TASK ADDED
MRBR REV.20
APPLICABILITY CHANGED FROM: "A330-200 OR
MRBR REV.20
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
ISSUE: JUL 01/21
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
ALI REV.04
MRBR REV.20
ALI REV.04
ALI REV.04
MRBR REV.20
APPLICABILITY REVIEW
ALI REV.04
MRBR REV.20
MRBR REV.20
MRBR REV.20, TASK
SPLIT TO 528104-01-4,
ALI REV.04
MRBR REV.20, TASK
SPLIT FROM 52810401-2
MRBR REV.20
Page 16
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
531112-02-1
3-53
531116-01-2
3-53
531118-01-1
3-53
531120-01-3
3-53
531120-01-4
3-53
531124-01-6
3-53
531124-01-7
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
GROUP 33A POST 40347 OR GROUP 33B OR
GROUP 33C OR GROUP 33D OR GROUP 33E OR
A330-900", TO: "A330-200 OR GROUP 33A POST
40347 OR GROUP 33B OR GROUP 33C OR GROUP
33D OR GROUP 33E OR A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-900", TO: "A330-200 OR A330300 OR A330-800 OR A330-900"
R FH OPTIMIZED 100% THRESHOLD: "6 YE OR 1600
FC OR 11100 FH" REMOVED
FH OPTIMIZED 100% INTERVAL: "6 YE OR 1600 FC
OR 11100 FH" REMOVED
FC OPTIMIZED 100% THRESHOLD: "6 YE OR 1800
FC" REMOVED
FC OPTIMIZED 100% INTERVAL: "6 YE OR 1800 FC"
REMOVED
100% THRESHOLD: "6 YE OR 1800 FC" ADDED
100% INTERVAL: "6 YE OR 1800 FC" ADDED
R IN SOURCE: "ALI" ADDED
IN SOURCEREFERENCE: "ALI 531120-01-03"
ADDED
100% THRESHOLD CHANGED FROM: "6 YE", TO: "6
YE OR 1800 FC"
100% INTERVAL CHANGED FROM: "6 YE", TO: "6
YE OR 1800 FC"
R APPLICABILITY CHANGED FROM: "GROUP 32A
POST 49194 OR GROUP 32E OR GROUP 33C POST
49194 OR GROUP 33D POST 49194 OR GROUP
33E OR A330-200F OR A330-900", TO: "GROUP
32A POST 49194 OR GROUP 32E OR GROUP 33C
POST 49194 OR GROUP 33D POST 49194 OR
GROUP 33E OR A330-200F OR A330-800 OR A330900"
D TASK DELETED
3-53
531135-01-2
R
ISSUE: JUL 01/21
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-900", TO: "A330-200 OR A330300 OR A330-800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
TASK WAS ALREADY
COVERED BY 53112401-6
ALI REV.04
Page 17
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
531154-01-3
3-53
531172-02-1
3-53
531175-01-4
3-53
531192-01-3
3-53
531194-01-3
3-53
532010-01-1
3-53
3-53
532010-01-3
532015-02-1
3-53
532021-01-1
3-53
3-53
3-53
532101-01-5
532101-02-4
532107-01-1
3-53
532115-01-1
3-53
532115-02-1
3-53
3-53
3-53
532117-01-7
532117-02-6
532124-02-12
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 32A
POST 49194 OR GROUP 32E OR GROUP 33C POST
49194 OR GROUP 33D POST 49194 OR GROUP
33E OR A330-200F OR A330-900", TO: "GROUP
32A POST 49194 OR GROUP 32E OR GROUP 33C
POST 49194 OR GROUP 33D POST 49194 OR
GROUP 33E OR A330-200F OR A330-800 OR A330900"
R IN REFERENCE(S): "AMT 531100-220-873; ISI
53.00.00106" ADDED AND "AMT 531100-200865" REMOVED
R APPLICABILITY CHANGED FROM: "A330-200F OR
GROUP 32E OR GROUP 33E OR A330-900", TO:
"A330-200F OR GROUP 32E OR GROUP 33E OR
A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 OR A330-900 PRE 207735"
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300 OR A330800 OR A330-900 PRE 207735"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-900", TO: "A330-200 OR A330300 OR A330-800 OR A330-900 PRE 207504"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-900", TO: "A330-200 OR A330300 OR A330-800 OR A330-900"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
AMM REFERENCE
REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
MRBR REV.20
MRBR REV.20
MRBR REV.20
APPLICABILITY REVIEW
ALI REV.04
MRBR REV.20
MRBR REV.20
ALI REV.04
Page 18
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
532125-01-11
3-53
532126-01-2
3-53
532130-01-5
3-53
532149-01-4
3-53
532149-01-5
3-53
532149-01-6
3-53
3-53
3-53
532166-01-5
532166-02-5
532189-01-2
3-53
532195-01-1
3-53
532195-01-2
3-53
532199-01-2
3-53
532199-01-3
3-53
533005-01-5
3-53
533005-01-8
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R DESCRIPTION CHANGED FROM: "INSPECTION
(MFEC &", TO: "INSPECTION (LFEC &"
R DESCRIPTION CHANGED FROM: "INSPECTION
(MFEC &", TO: "INSPECTION (LFEC &"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "27900 FC OR 180000 FH", TO: "27900 FC
OR 189600 FH"
R DESCRIPTION CHANGED FROM: "INSPECTION
(MFEC &", TO: "INSPECTION (LFEC &"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "30100 FC OR 180000 FH", TO: "30100 FC
OR 204200 FH"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 OR
GROUP 33C OR GROUP 33D OR GROUP 33E OR
A330-900", TO: "A330-200 OR GROUP 33C OR
GROUP 33D OR GROUP 33E OR A330-800 OR
A330-900 PRE 207504"
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "28000 FC OR 190000 FH", TO: "28000 FC
OR 190200 FH"
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R APPLICABILITY CHANGED FROM: "GROUP 32A",
TO: "GROUP 32A OR A330-900"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
MRBR REV.20
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
MRBR REV.20
MRBR REV.20
Page 19
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533015-02-1
3-53
533016-01-2
3-53
533016-01-6
3-53
3-53
3-53
533016-01-7
533016-01-8
533029-01-2
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
GROUP 33A POST 42418 S11929 OR GROUP 33B
OR GROUP 33C OR GROUP 33D OR GROUP 33E OR
A330-900", TO: "A330-200 OR GROUP 33A POST
42418 S11929 OR GROUP 33B OR GROUP 33C OR
GROUP 33D OR GROUP 33E OR A330-800 OR
A330-900 OR A330-200F"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "31100 FC OR 210500 FH", TO: "26100 FC
OR 177200 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"5400 FC OR 37000 FH", TO: "3800 FC OR 25900
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "39200 FC OR 117600 FH", TO: "33000 FC
OR 99000 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6100 FC OR 19900 FH", TO: "4200 FC OR 14000
FH"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "31800 FC OR 180000 FH", TO: "26700 FC
OR 181200 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"5500 FC OR 37800 FH", TO: "3900 FC OR 26500
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "40100 FC OR 120300 FH", TO: "33700 FC
OR 101300 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6200 FC OR 20400 FH", TO: "4300 FC OR 14300
FH"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 OR
GROUP 33C OR GROUP 33D OR GROUP 33E OR
A330-900", TO: "A330-200 OR GROUP 33C OR
GROUP 33D OR GROUP 33E OR A330-800 OR
A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 20
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533031-01-1
3-53
533031-01-2
3-53
533031-01-3
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "30900 FC OR 209400 FH", TO: "27500 FC
OR 186500 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4500 FC OR 31000 FH", TO: "3300 FC OR 22800
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "39000 FC OR 117000 FH", TO: "34700 FC
OR 104200 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5100 FC OR 16700 FH", TO: "3700 FC OR 12300
FH"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "26400 FC OR 178700 FH", TO: "23400 FC
OR 158300 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4700 FC OR 32000 FH", TO: "3400 FC OR 23500
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "33200 FC OR 99800 FH", TO: "29500 FC
OR 88500 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5200 FC OR 17200 FH", TO: "3800 FC OR 12700
FH"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "27000 FC OR 182700 FH", TO: "23800 FC
OR 161600 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4700 FC OR 32000 FH", TO: "3700 FC OR 25100
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "34000 FC OR 102100 FH", TO: "30100 FC
OR 90300 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5200 FC OR 17200 FH", TO: "4100 FC OR 13500
FH"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
Page 21
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533031-01-4
3-53
533031-01-5
3-53
3-53
3-53
533031-01-6
533031-01-7
533031-01-8
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "31600 FC OR 214000 FH", TO: "28000 FC
OR 189800 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"5400 FC OR 36700 FH", TO: "3900 FC OR 26900
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "39800 FC OR 119600 FH", TO: "35300 FC
OR 106000 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6000 FC OR 19800 FH", TO: "4400 FC OR 14500
FH"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "23400 FC OR 158900 FH", TO: "20700 FC
OR 140700 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4500 FC OR 30500 FH", TO: "3300 FC OR 22300
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "29600 FC OR 88800 FH", TO: "26200 FC
OR 78600 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5000 FC OR 16400 FH", TO: "3600 FC OR 12000
FH"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "GROUP 32E PRE
50166 S16571", TO: "GROUP 32E PRE 50166"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "25800 FC OR 174600 FH", TO: "22900 FC
OR 155000 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4200 FC OR 28500 FH", TO: "3000 FC OR 20800
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "31800 FC OR 111600 FH", TO: "28300 FC
OR 99000 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"4600 FC OR 16400 FH", TO: "3400 FC OR 12000
FH"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 22
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533031-01-9
3-53
3-53
3-53
533032-01-7
533052-09-1
533072-02-1
3-53
533072-02-2
3-53
533072-02-3
3-53
3-53
3-53
533078-01-3
533078-01-4
533080-01-1
3-53
3-53
3-53
533106-01-8
533106-02-6
533107-01-3
3-53
533107-02-2
3-53
533107-02-3
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "21700 FC OR 147300 FH", TO: "19200 FC
OR 130200 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"4400 FC OR 30400 FH", TO: "3300 FC OR 22300
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "27400 FC OR 82300 FH", TO: "24200 FC
OR 72800 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5000 FC OR 16400 FH", TO: "3600 FC OR 12000
FH"
N NEW TASK ADDED
N NEW TASK ADDED
R DESCRIPTION CHANGED FROM: "(US) OF", TO:
"(US + ROTOTEST) OF"
IN PREPARATION TASKS: "BOLTS" ADDED
R DESCRIPTION CHANGED FROM: "(US) OF", TO:
"(US + ROTOTEST) OF"
IN PREPARATION TASKS: "BOLTS" ADDED
R DESCRIPTION CHANGED FROM: "(US) OF", TO:
"(US + ROTOTEST) OF"
IN PREPARATION TASKS: "BOLTS" ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900 PRE 207464 OR A330900 PRE 207465"
N NEW TASK ADDED
N NEW TASK ADDED
R IN SOURCE: "ALI WFD" ADDED AND "ALI"
REMOVED
IN SOURCEREFERENCE: "ALI WFD 533107-01-03"
ADDED AND "ALI 533107-01-03" REMOVED
IN REFERENCE(S): "ALI WFD 533107-01-03"
ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207401"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 23
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533125-01-3
3-53
533125-01-5
3-53
3-53
3-53
533126-01-8
533127-03-7
533164-01-9
3-53
533180-02-2
3-53
3-53
533186-02-2
533187-01-3
3-53
533187-01-5
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 33B OR
GROUP 32E POST 41652 S11927 OR GROUP 33E
POST 41652 S11927 OR A330-900", TO: "GROUP
33B OR GROUP 32E POST 41652 S11927 OR
GROUP 33E POST 41652 S11927 OR A330-800 OR
A330-900"
R APPLICABILITY CHANGED FROM: "GROUP 32E PRE
41652 S11927 OR GROUP 33E PRE 41652 S11927
OR A330-800", TO: "GROUP 32E PRE 41652
S11927 OR GROUP 33E PRE 41652 S11927"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "18500 FC OR 124800 FH", TO: "16500 FC
OR 111400 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "22900 FC OR 68800 FH", TO: "20400 FC
OR 61400 FH"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "GROUP 33C OR
GROUP 33D", TO: "GROUP 33C OR GROUP 33D OR
GROUP 33E"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "19900 FC OR 62400 FH", TO: "19900 FC
OR 59900 FH"
D TASK DELETED
3-53
3-53
533193-01-6
533193-02-1
N
R
3-53
3-53
3-53
533193-02-3
533194-01-20
533194-01-21
N
N
N
ISSUE: JUL 01/21
NEW TASK ADDED
FH OPTIMIZED 100% THRESHOLD: "17000 FC"
ADDED
FH OPTIMIZED 100% INTERVAL: "6100 FC OR
39700 FH" ADDED
FC OPTIMIZED 100% THRESHOLD: "17000 FC"
ADDED
FC OPTIMIZED 100% INTERVAL: "6800 FC OR
24200 FH" ADDED
100% THRESHOLD: "17000 FC" REMOVED
100% INTERVAL: "6900 FC" REMOVED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
TASK SPLIT TO 53312501-3
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04, TASK
CONSOLDATION WITH
533187-01-5
ALI REV.04, TASK
CONSOLIDATED WITH
533187-01-3
MRBR REV.20
MRBR REV.20
MRBR REV.20
ALI REV.04
ALI REV.04
Page 24
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
3-53
3-53
533195-02-13
533195-02-15
533197-01-1
M
V
T
N
N
R
3-53
533197-01-2
D
3-53
533197-02-1
R
3-53
533197-02-2
D
3-53
533198-01-2
R
3-53
533201-01-2
R
3-53
533202-01-1
R
3-53
533202-01-2
R
3-53
533202-01-3
R
ISSUE: JUL 01/21
DESCRIPTION
NEW TASK ADDED
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-200F OR
A330-300 OR A330-800 OR A330-900"
TASK DELETED
APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-200F OR
A330-300 OR A330-800 OR A330-900"
TASK DELETED
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900 PRE 207465"
APPLICABILITY CHANGED FROM: "A330-200 PRE
204416 (53-3236) DOOR TYPE A", TO: "A330-200
PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
APPLICABILITY CHANGED FROM: "GROUP 33B PRE
204416 (53-3236) DOOR TYPE A OR GROUP 33C
PRE 204416 (53-3236) DOOR TYPE A OR GROUP
33D PRE 204416 (53-3236) DOOR TYPE A OR
GROUP 33E PRE 204416 (53-3236) DOOR TYPE
A", TO: "GROUP 33B PRE 204416 (53-3236) PRE
207278 (53-3291) DOOR TYPE A OR GROUP 33C
PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A OR GROUP 33D PRE 204416 (533236) PRE 207278 (53-3291) DOOR TYPE A OR
GROUP 33E PRE 204416 (53-3236) PRE 207278
(53-3291) DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
APPLICABILITY CHANGED FROM: "GROUP 33A PRE
204416 (53-3236) DOOR TYPE A", TO: "GROUP
33A PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
MRBR REV.20, TASK
CONSOLIDATION WITH
533197-01-2
MRBR REV.20, TASK
CONSOLIDATED WITH
533197-01-1
MRBR REV.20, TASK
CONSOLIDATION WITH
533197-02-2
MRBR REV.20, TASK
CONSOLIDATED WITH
533197-02-1
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 25
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
533203-01-1
3-53
533203-01-2
3-53
533203-01-3
3-53
534006-01-1
3-53
534007-01-1
3-53
534007-02-1
3-53
534008-01-1
3-53
534012-01-2
3-53
534013-01-2
3-53
534014-02-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 PRE
204416 (53-3236) DOOR TYPE A", TO: "A330-200
PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
R APPLICABILITY CHANGED FROM: "GROUP 33B PRE
204416 (53-3236) DOOR TYPE A OR GROUP 33C
PRE 204416 (53-3236) DOOR TYPE A OR GROUP
33D PRE 204416 (53-3236) DOOR TYPE A OR
GROUP 33E PRE 204416 (53-3236) DOOR TYPE
A", TO: "GROUP 33B PRE 204416 (53-3236) PRE
207278 (53-3291) DOOR TYPE A OR GROUP 33C
PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A OR GROUP 33D PRE 204416 (533236) PRE 207278 (53-3291) DOOR TYPE A OR
GROUP 33E PRE 204416 (53-3236) PRE 207278
(53-3291) DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
R APPLICABILITY CHANGED FROM: "GROUP 33A PRE
204416 (53-3236) DOOR TYPE A", TO: "GROUP
33A PRE 204416 (53-3236) PRE 207278 (53-3291)
DOOR TYPE A"
DESCRIPTION CHANGED FROM: "INSPECTION
(HFEC & LFEC) OF", TO: "INSPECTION (LFEC) OF"
R APPLICABILITY CHANGED FROM: "GROUP 33A PRE
204638 OR GROUP 33B PRE 44593 PRE 204638",
TO: "GROUP 33A PRE 204638 (53-3257) OR
GROUP 33B PRE 44593 PRE 204638 (53-3257)"
R APPLICABILITY CHANGED FROM: "GROUP 33A PRE
204638 OR GROUP 33B PRE 44203 PRE 204638",
TO: "GROUP 33A PRE 204638 (53-3257) OR
GROUP 33B PRE 44593 PRE 204638 (53-3257)"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R DESCRIPTION CHANGED FROM: "(US) OF", TO:
"(US + HFEC) OF"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
MOD SB REVIEW
MOD SB REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 26
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
534017-01-1
3-53
534017-01-2
3-53
534017-02-1
3-53
534017-02-2
3-53
534108-02-5
3-53
3-53
3-53
3-53
3-53
3-53
3-53
3-53
534120-01-7
534124-01-5
534124-02-4
534126-01-5
534126-02-4
534131-01-5
534132-02-5
534137-01-5
3-53
534139-01-3
3-53
534139-02-2
3-53
534140-02-5
3-53
534143-02-2
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 PRE 209293 OR A330300 PRE 209293"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 PRE 209293 OR A330-900 PRE 207505
PRE 209293"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "27400 FC OR 177800 FH", TO: "12300 FC
OR 81300 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "31300 FC OR 110400 FH", TO: "14300 FC
OR 50500 FH"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330200F"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 PRE 209293 OR A330-900 PRE 207505
PRE 209293"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R IN SOURCE: "ALI" ADDED
IN SOURCEREFERENCE: "ALI 534140-02-03"
ADDED
100% THRESHOLD CHANGED FROM: "6 YE", TO: "6
YE OR 2600 FC"
100% INTERVAL CHANGED FROM: "6 YE", TO: "6
YE OR 2600 FC"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
APPLICABILITY REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
Page 27
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
534144-01-2
3-53
534144-03-2
3-53
534146-01-1
3-53
534149-01-1
3-53
534149-02-2
3-53
534149-02-3
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 32A OR
GROUP 33A OR GROUP 33B OR GROUP 33C OR
GROUP 33D", TO: "GROUP 32A OR GROUP 33A OR
GROUP 33B OR GROUP 33C OR GROUP 33D OR
GROUP 38E OR GROUP 39E"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "ALL"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 PRE 208052 OR A330-900 PRE
207505"
N NEW TASK ADDED
3-53
534154-01-5
R
3-53
534156-01-1
R
3-53
534166-02-1
R
3-53
3-53
3-53
534177-01-5
534177-02-5
534178-01-2
N
N
R
3-53
534178-01-3
R
3-53
534178-01-6
R
3-53
534179-01-3
N
ISSUE: JUL 01/21
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
APPLICABILITY CHANGED FROM: "GROUP 32A OR
GROUP 32E OR GROUP 32F OR GROUP 33B POST
44203 OR GROUP 33C OR GROUP 33D OR GROUP
33E", TO: "GROUP 32A OR GROUP 32E OR GROUP
32F OR GROUP 33B POST 44203 OR GROUP 33C
OR GROUP 33D OR GROUP 33E OR GROUP 38E OR
GROUP 39E"
DESCRIPTION CHANGED FROM: "INSPECTION OF",
TO: "INSPECTION (US) OF"
100% INTERVAL CHANGED FROM: "18000 FC", TO:
"18100 FC"
NEW TASK ADDED
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "GROUP 33A
POST 40556 PRE 204503 (53-3259)", TO: "GROUP
33A POST 40556 PRE 204503 (53-3259) PRE
207253 (53-3288)"
APPLICABILITY CHANGED FROM: "GROUP 33B PRE
44593 PRE 204503 (53-3259)", TO: "GROUP 33B
PRE 44593 PRE 204503 (53-3259) PRE 207253
(53-3288)"
APPLICABILITY CHANGED FROM: "GROUP 32A PRE
204503 (53-3259)", TO: "GROUP 32A PRE 204503
(53-3259) PRE 207253 (53-3288)"
NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
APPLICABILITY REVIEW
ALI REV.04
APPLICABILITY REVIEW
APPLICABILITY REVIEW
ALI REV.04, MRBR
REV.20
MRBR REV.20, ALI
REV.04
ALI REV.04
APPLICABILITY REVIEW
ALI REV.04
MRBR REV.20
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 28
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
3-53
534179-01-6
534179-01-8
3-53
3-53
534179-01-1
534182-01-1
3-53
534187-01-1
3-53
534187-01-2
3-53
534187-01-3
3-53
534187-01-4
3-53
534187-01-5
3-53
534187-01-6
3-53
534187-01-7
3-53
534188-01-1
3-53
534188-01-2
ISSUE: JUL 01/21
M
V DESCRIPTION
T
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200F PRE
204678 (53-3256)", TO: "A330-200F PRE 204678
(53-3256) PRE 207235 (53-3289)"
D TASK DELETED
R DESCRIPTION CHANGED FROM: "(HFEC) OF", TO:
"(HFEC + US) OF"
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM" ADDED
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "29900 FC OR 180000 FH", TO: "26500 FC
OR 158600 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "33400 FC OR 100200 FH", TO: "29200 FC
OR 87800 FH"
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM" ADDED
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"15800 FC", TO: "15300 FC"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"17600 FC", TO: "15300 FC"
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R TASK NOTE "ROTO TEST INSPECTION TO BE
PERFORMED IN CASE US INSPECTION IS NOT
FEASIBLE ACCORDING TO NTM." ADDED
R APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-300 OR A330-200F"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 29
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-53
535109-01-1
3-53
3-53
535109-01-3
535133-01-1
3-53
3-53
535133-01-2
535134-01-1
3-53
3-54
533015-03-6
545174-01-10
3-54
545174-01-14
3-54
545174-01-15
3-54
545174-01-4
3-54
545174-02-10
3-54
545174-02-11
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300 OR A330-900", TO: "A330-200 OR A330300"
IN ZONE "311" ACCESS MH CHANGED FROM:
"5.42", TO: "0.02"
IN ZONE "311" ACCESS "331AT; 333AB; 333AT"
REMOVED
IN ZONE "312" ACCESS MH CHANGED FROM:
"5.41", TO: ""
IN ZONE "312" ACCESS "312AR; 341AT; 343AB;
343AT" REMOVED
N NEW TASK ADDED
R IN PREPARATION MH : "TBD" ADDED
IN PREPARATION TASKS: "BOLTS" ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200", TO:
"A330-200 OR A330-800"
D TASK DELETED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
TASK SPLIT TO 53510901-3, ACCESS REVIEW
ALI REV.04
PREPARATION REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
Page 30
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-54
545174-02-12
3-54
545174-02-14
3-54
545174-02-15
3-54
545174-02-2
3-54
545174-02-3
3-54
545174-02-4
3-54
545174-02-5
3-54
545174-02-9
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
R IN PREPARATION MH : "36.00" ADDED
IN PREPARATION TASKS: "BEARINGS; ENGINE;
LINKS" ADDED
IN REFERENCE(S): "AMT 545117-220-806" ADDED
AND "AMT 545117-200-812" REMOVED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
PREPARATION
REVIEW, AMM
REFERENCE REVIEW
Page 31
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-54
545410-01-1
3-54
545411-01-1
3-54
545412-01-1
3-54
545413-01-1
3-54
545414-01-1
3-54
545415-01-1
3-54
545416-01-1
3-54
545418-01-1
3-54
545419-01-1
3-54
545420-01-1
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
551001-02-1
551001-02-2
551001-02-3
551004-02-1
551004-02-2
551008-02-1
551008-02-2
551008-02-3
551008-02-4
551013-02-5
551015-02-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 545410-01-2"
ADDED
100% THRESHOLD CHANGED FROM: "12 YE", TO:
"12 YE OR 17000 FC OR 50000 FH"
100% INTERVAL CHANGED FROM: "12 YE", TO:
"12 YE OR 8000 FC OR 25000 FH"
R IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 545411-01-2"
ADDED
100% THRESHOLD CHANGED FROM: "12 YE", TO:
"12 YE OR 17000 FC OR 50000 FH"
100% INTERVAL CHANGED FROM: "12 YE", TO:
"12 YE OR 8000 FC OR 25000 FH"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
DESCRIPTION CHANGED FROM: "INSPECTION (US)
OF", TO: "INSPECTION (HFEC) OF"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
MRBR REV.20
ALI REV.04
Page 32
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
3-55
551015-02-2
551015-02-3
551015-02-4
551015-02-5
551015-03-1
551015-03-2
551015-03-3
551015-03-4
551015-03-5
551016-01-10
551016-01-6
M
V
T
N
N
N
N
N
N
N
N
N
N
R
3-55
551016-01-8
R
3-55
3-55
551016-01-9
551016-01-7
N
D
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "GROUP 33A",
TO: "GROUP 33A OR GROUP 33B"
TASK NOTE "PLANNING: FOR GROUP 33B, CREDIT
CAN BE TAKEN FROM INSPECTIONS PERFORMED
ACCORDING TO TASK 551016-01-7" ADDED
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "26500 FC OR 179700 FH", TO: "12500 FC
OR 75000 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"22100 FC OR 149600 FH", TO: "2000 FC OR
12100 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "32400 FC OR 97400 FH", TO: "15400 FC
OR 46200 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"31600 FC OR 94800 FH", TO: "2500 FC OR 7500
FH"
APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
NEW TASK ADDED
TASK DELETED
3-55
3-55
3-55
3-55
551019-01-4
551028-03-1
551028-03-2
551028-03-3
D
N
N
N
TASK DELETED
NEW TASK ADDED
NEW TASK ADDED
NEW TASK ADDED
ISSUE: JUL 01/21
DESCRIPTION
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04, TASK
CONSOLIDATION WITH
551016-01-7
ALI REV.04
ALI REV.04
ALI REV.04, TASK
CONSOLIDATED WITH
551016-01-6
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 33
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-55
551032-01-1
3-55
551032-01-10
3-55
551032-01-11
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200F", TO:
"GROUP 32F POST 44037 PRE 205928"
100% THRESHOLD CHANGED FROM: "6 YE OR
16300 FC OR 49500 FH", TO: "6 YE OR 16800 FC
OR 51000 FH"
100% INTERVAL CHANGED FROM: "6 YE OR 3800
FC OR 11700 FH", TO: "6 YE OR 7400 FC OR 22600
FH"
R APPLICABILITY CHANGED FROM: "GROUP 33C",
TO: "GROUP 33C POST 44037 OR GROUP 33D
POST 44037"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 25500 FC OR 153100 FH", TO: "6
YE OR 29000 FC OR 174300 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 13200 FC OR 79700 FH", TO: "6 YE OR
16300 FC OR 97900 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 29700 FC OR 89300 FH", TO: "6
YE OR 30700 FC OR 92200 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 15800 FC OR 47600 FH", TO: "6 YE OR
17500 FC OR 52500 FH"
R APPLICABILITY CHANGED FROM: "GROUP 33E",
TO: "GROUP 33E POST 44037 PRE 205928"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 17500 FC OR 105200 FH", TO: "6
YE OR 24700 FC OR 148300 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 9300 FC OR 56300 FH", TO: "6 YE OR
13000 FC OR 78400 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 20400 FC OR 61400 FH", TO: "6
YE OR 26100 FC OR 78400 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 11200 FC OR 33600 FH", TO: "6 YE OR
14000 FC OR 42000 FH"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
Page 34
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-55
551032-01-13
3-55
3-55
3-55
551032-01-15
551032-01-17
551032-01-2
3-55
551032-01-8
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 33A
POST 42133 OR GROUP 33B POST 42133", TO:
"GROUP 33A POST 42133 PRE 44037 OR GROUP
33B POST 42133 PRE 44037"
IN SOURCE: "ALI" ADDED
IN SOURCEREFERENCE: "ALI 551032-01-16"
ADDED
FH OPTIMIZED 100% THRESHOLD: "6 YE OR 21900
FC OR 131800 FH" ADDED
FH OPTIMIZED 100% INTERVAL: "6 YE OR 11200
FC OR 67200 FH" ADDED
FC OPTIMIZED 100% THRESHOLD: "6 YE OR 23000
FC OR 69200 FH" ADDED
FC OPTIMIZED 100% INTERVAL: "6 YE OR 11900 FC
OR 35700 FH" ADDED
100% THRESHOLD: "6 YE" REMOVED
100% INTERVAL: "6 YE" REMOVED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "GROUP 33A PRE
42133 OR GROUP 33B PRE 42133 OR GROUP
33D", TO: "GROUP 32A PRE 44037 OR GROUP
33A PRE 42133 OR GROUP 33B PRE 42133 OR
GROUP 33C PRE 44037 OR GROUP 33D PRE
44037"
R APPLICABILITY CHANGED FROM: "GROUP 32A",
TO: "GROUP 32A POST 44037"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 24500 FC OR 159200 FH", TO: "6
YE OR 24100 FC OR 157100 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 7000 FC OR 45700 FH", TO: "6 YE OR
13300 FC OR 86400 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 31800 FC OR 111300 FH", TO: "6
YE OR 26800 FC OR 93900 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 9300 FC OR 32600 FH", TO: "6 YE OR
14900 FC OR 52200 FH"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 35
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-55
551032-01-9
3-55
3-55
3-55
3-55
3-55
3-57
551008-01-4
551008-01-6
551008-01-7
551015-01-4
551024-01-4
571112-01-1
3-57
3-57
3-57
3-57
3-57
571112-01-2
571112-01-4
571123-01-8
571123-01-9
571125-01-9
3-57
571132-02-4
3-57
571133-01-7
3-57
3-57
3-57
571133-01-8
571133-02-1
571144-01-9
3-57
571146-02-10
3-57
3-57
571146-02-11
571153-01-2
3-57
571159-01-10
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 32E",
TO: "GROUP 32E POST 44037 PRE 205928"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 14200 FC OR 92800 FH", TO: "6
YE OR 20400 FC OR 132600 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 3700 FC OR 24000 FH", TO: "6 YE OR
10300 FC OR 67000 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "6 YE OR 18500 FC OR 64800 FH", TO: "6
YE OR 22600 FC OR 79200 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"6 YE OR 4900 FC OR 17200 FH", TO: "6 YE OR
11500 FC OR 40500 FH"
D TASK DELETED
D TASK DELETED
D TASK DELETED
D TASK DELETED
D TASK DELETED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207401"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900 PRE 207401"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207401"
N NEW TASK ADDED
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900 PRE 207401"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "GROUP 32E",
TO: "GROUP 32E OR A330-800"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 36
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
571164-01-3
3-57
571170-01-1
3-57
3-57
571171-01-2
571171-01-3
3-57
571173-01-1
3-57
571174-01-6
3-57
571179-01-1
3-57
571180-03-1
3-57
3-57
3-57
3-57
3-57
3-57
571180-03-2
571180-03-3
572012-02-10
572012-02-9
572032-01-15
572046-02-1
3-57
572046-02-11
3-57
572046-02-4
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "GROUP 32E PRE
55306 OR GROUP 33E PRE 55306", TO: "GROUP
32A OR GROUP 33A OR GROUP 33B OR GROUP
33C OR GROUP 33D OR GROUP 32E PRE 55306
OR GROUP 33E PRE 55306"
N NEW TASK ADDED
R FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "20000 FC OR 120500 FH", TO: "17800 FC
OR 106800 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"11600 FC OR 69800 FH", TO: "10800 FC OR
65000 FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "24600 FC OR 73800 FH", TO: "21800 FC
OR 65400 FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"13600 FC OR 40800 FH", TO: "12600 FC OR
38000 FH"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900 PRE 207401"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207401"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
MRBR REV.20
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
Page 37
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
572046-02-5
3-57
572046-02-6
3-57
572046-02-7
3-57
572046-02-8
3-57
572046-02-9
3-57
572047-02-1
3-57
3-57
572047-02-2
572051-01-15
3-57
3-57
572051-01-16
572052-03-12
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207878"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "22700 FC OR 138000 FH", TO: "23000 FC
OR 138000 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"3200 FC OR 20100 FH", TO: "3300 FC OR 20100
FH"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207878"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "17500 FC OR 106500 FH", TO: "17700 FC
OR 106500 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"2500 FC OR 16100 FH", TO: "2600 FC OR 16100
FH"
N NEW TASK ADDED
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
PREPARATION REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
Page 38
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
572054-01-17
3-57
3-57
3-57
3-57
3-57
572054-01-18
572081-02-2
572082-01-16
572083-01-10
572083-01-8
3-57
572083-01-9
3-57
572086-01-1
3-57
572119-02-1
3-57
572119-02-5
3-57
572119-02-7
3-57
572119-02-8
3-57
572119-02-9
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207878"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "19400 FC OR 118200 FH", TO: "19700 FC
OR 118200 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"3600 FC OR 23800 FH", TO: "5700 FC OR 34400
FH"
FC OPTIMIZED 100% INTERVAL CHANGED FROM:
"5300 FC OR 16100 FH", TO: "7500 FC OR 22500
FH"
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
N NEW TASK ADDED
R IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R APPLICABILITY CHANGED FROM: "A330-800 OR
A330-200F", TO: "A330-200F"
IN PREPARATION MH : "2.00" ADDED
IN PREPARATION TASKS: "FUEL TANK DRAINED
AND VENTED" ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-800 OR A330-900"
R IN SOURCEREFERENCE: "(CPCP) MRB SSI 57211902-11; (CPCP) MRB SSI 572119-02-2; (CPCP) MRB
SSI 572119-02-3; (CPCP) MRB SSI 572119-02-4"
REMOVED
R IN SOURCEREFERENCE: "(CPCP) MRB SSI 57211902-1" ADDED AND "(CPCP) MRB SSI 572119-02-5"
REMOVED
R IN SOURCEREFERENCE: "(CPCP) MRB SSI 57211902-1" ADDED AND "(CPCP) MRB SSI 572119-02-7"
REMOVED
R IN SOURCEREFERENCE: "(CPCP) MRB SSI 57211902-1" ADDED AND "(CPCP) MRB SSI 572119-02-8"
REMOVED
R IN SOURCEREFERENCE: "(CPCP) MRB SSI 57211902-1" ADDED AND "(CPCP) MRB SSI 572119-02-9"
REMOVED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
PREPARATION REVIEW
TASK SPLIT TO 57208301-10, PREPARATION
REVIEW
ALI REV.04
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
MRBR REV.20
Page 39
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
572149-01-4
3-57
572154-01-10
3-57
572404-01-1
3-57
3-57
572404-01-2
572404-02-1
3-57
3-57
3-57
572404-02-2
572413-01-2
573001-09-1
3-57
574106-01-6
3-57
574109-02-9
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-200F OR A330-300", TO: "A330-200 OR
A330-200F OR A330-300 OR A330-800 OR A330900"
IN SOURCEREFERENCE: "(CPCP) MRB SSI 57214901-12; (CPCP) MRB SSI 572149-01-5; (CPCP) MRB
SSI 572149-01-6; (CPCP) MRB SSI 572149-01-7;
(CPCP) MRB SSI 572149-01-9" REMOVED
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207766"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "19000 FC OR 114000 FH", TO: "22500 FC
OR 135000 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"9000 FC OR 54900 FH", TO: "9100 FC OR 54900
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "23200 FC OR 69700 FH", TO: "27500 FC
OR 82600 FH"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-900", TO:
"A330-900 PRE 207766"
DESCRIPTION CHANGED FROM: "ROTO ) OF", TO:
"ROTO) OF"
FH OPTIMIZED 100% THRESHOLD CHANGED
FROM: "19000 FC OR 114000 FH", TO: "22500 FC
OR 135000 FH"
FH OPTIMIZED 100% INTERVAL CHANGED FROM:
"9000 FC OR 54900 FH", TO: "9100 FC OR 54900
FH"
FC OPTIMIZED 100% THRESHOLD CHANGED
FROM: "23200 FC OR 69700 FH", TO: "27500 FC
OR 82600 FH"
N NEW TASK ADDED
N NEW TASK ADDED
R IN REFERENCE(S): "AMT 573000-280-804" ADDED
AND "AMT 573000-280-801" REMOVED
R FH OPTIMIZED SAMPLE INTERVAL CHANGED
FROM: "12 YE OR 20000 FC OR 60000 FH", TO: "12
YE OR 17500 FC OR 60000 FH"
N NEW TASK ADDED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
APPLICABILITY REVIEW
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
ALI REV.04
AMM REFERENCE
REVIEW
SAMPLE INTERVAL
REVIEW
MPD CORRECTION
Page 40
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
574115-02-6
3-57
574804-02-6
3-57
3-57
575011-01-15
575055-01-1
3-57
575059-01-1
3-57
575061-01-1
3-57
575067-01-2
3-57
575067-02-2
3-57
575069-01-2
3-57
575401-01-2
3-57
575401-02-1
3-57
575503-01-1
3-57
575503-02-1
3-57
575505-01-1
3-57
575505-02-1
3-57
575507-01-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "GROUP 32E",
TO: "GROUP 32E OR GROUP 38E OR GROUP 39E"
R APPLICABILITY CHANGED FROM: "A330-200F", TO:
"A330-200F OR A330-800 OR A330-900"
N NEW TASK ADDED
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
APPLICABILITY REVIEW
APPLICABILITY REVIEW
ALI REV.04
APPLICABILITY REVIEW
APPLICABILITY REVIEW
APPLICABILITY REVIEW
APPPLICABILITY
REVIEW
APPLICABILITY REVIEW
APPLICABILITY REVIEW
MRBR REV.20
MRBR REV.20
APPLICABILITY REVIEW
APPLICABILITY REVIEW
APPLICABILITY REVIEW
APPLICABILITY REVIEW
APPLICABILITY REVIEW
Page 41
MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-57
575507-02-1
3-57
576117-01-1
3-57
576117-01-2
3-57
576117-01-3
3-57
576117-01-4
M
V DESCRIPTION
T
R APPLICABILITY CHANGED FROM: "A330-200 OR
A330-300", TO: "A330-200 OR A330-300 OR A330800 OR A330-900"
R IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 576117-01-3"
ADDED
100% INTERVAL CHANGED FROM: "8700 FC OR
64400 FH", TO: "8700 FC OR 62700 FH"
R APPLICABILITY CHANGED FROM: "A330-200F OR
A330-200 POST 54708 OR A330-300 POST 54708",
TO: "A330-200 POST 54708 OR A330-300 POST
54708"
R IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 576117-01-2"
ADDED
N NEW TASK ADDED
3-57
3-57
576117-01-5
576120-01-1
N
R
3-57
576120-01-3
N
3-71
3-71
3-71
3-78
712142-01-2
712242-01-2
712243-01-2
783236-01-1
N
N
N
R
3-78
783239-01-1
R
ISSUE: JUL 01/21
NEW TASK ADDED
APPLICABILITY CHANGED FROM: "ALL", TO:
"A330-200 OR A330-200F OR A330-300"
IN SOURCE: "MRB" ADDED
IN SOURCEREFERENCE: "MRB SSI 576120-01-1;
MRB SSI 576120-01-2" ADDED
100% THRESHOLD CHANGED FROM: "18100 FC
OR 85500 FH", TO: "18000 FC OR 85500 FH"
100% INTERVAL CHANGED FROM: "12200 FC OR
57400 FH", TO: "8900 FC OR 26700 FH"
NEW TASK ADDED
REASON /
JUSTIFICATION
APPLICABILITY REVIEW
MRBR REV.20
MRBR REV.20, TASK
SPLIT TO 576117-01-4
MRBR REV.20
MRBR REV.20, TRASK
SPLIT FROM 57611701-2
MRBR REV.20
TASK SPLIT TO 57612001-3, MRBR REV.20,
ALI REV.04
MRBR REV.20, TASK
SPLIT FORM 57612001-1
NEW TASK ADDED
MRBR REV.20
NEW TASK ADDED
MRBR REV.20
NEW TASK ADDED
MRBR REV.20
100% THRESHOLD CHANGED FROM: "6 YE", TO: "6 MRBR REV.20
YE OR 14500 FC OR 43500 FH"
100% INTERVAL CHANGED FROM: "6 YE", TO: "6
YE OR 14500 FC OR 43500 FH"
100% THRESHOLD CHANGED FROM: "12 YE", TO:
MRBR REV.20
"12 YE OR 14800 FC OR 44400 FH"
100% INTERVAL CHANGED FROM: "12 YE", TO:
"12 YE OR 14800 FC OR 44400 FH"
SUMMARY OF CHANGES
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MAINTENANCE PLANNING DOCUMENT
MPD
SEC
TASK NUMBER
3-78
783240-01-1
3-78
4-ZL/500
783243-01-1
ZL-573-01-1
ISSUE: JUL 01/21
M
V DESCRIPTION
T
R 100% THRESHOLD CHANGED FROM: "12 YE", TO:
"12 YE OR 10400 FC OR 31200 FH"
100% INTERVAL CHANGED FROM: "12 YE", TO:
"12 YE OR 10400 FC OR 31200 FH"
N NEW TASK ADDED
R IN ZONE "573" ACCESS MH CHANGED FROM:
"1.25", TO: "0.35"
IN ZONE "573" ACCESS "573CB; 573GB" ADDED
AND "573EB; 573FB" REMOVED
IN ZONE "673" ACCESS MH CHANGED FROM:
"1.25", TO: "0.35"
IN ZONE "673" ACCESS "673CB; 673GB" ADDED
AND "673EB; 673FB" REMOVED
SUMMARY OF CHANGES
REASON /
JUSTIFICATION
MRBR REV.20
MRBR REV.20
ACCESS REVIEW
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MAINTENANCE PLANNING DOCUMENT
GENERAL INTRODUCTION
1. SCOPE, VALIDITY AND LIMITATIONS
A. GENERAL
The A330 Maintenance Planning Document (MPD) is an AIRBUS envelope repository document
which provides a direct access to repetitive maintenance tasks published in the MRB Report (MRBR),
the Airworthiness Limitation Section (ALS) Parts 2, 3, 4 and 5 and the ETOPS CMP Documents and
provides additional information about maintenance tasks, their scheduling and procedures.
Maintenance requirements promulgated through ALS Part 1, ALS Part 2 (Section 4), ALS Part 4
(Section 3) and ALS Part 5 (Section 3 and 5) are not included in MPD since they are not repetitive
maintenance tasks or have a threshold beyond the MPPT (ALS Part 2). However these mandatory
requirements approved by Primary Type Certification Authorities shall be addressed by Operators
Maintenance Programs.
The MPD itself is not an ICA document, but contains ICA information based on published ICA
documents (i.e. MRBR, ALS Parts, ETOPS CMP) and refers to ICA information covered in the
Aircraft Maintenance Manual (AMM).
It may be used by operators to develop their locally approved scheduled maintenance programs.
All MRBR and ALS tasks are declared as Instructions for Continued Airworthiness (ICA) and when
applicable to the aircraft configuration should be included in the operator’s initial maintenance
program.
MRBR tasks and intervals constitute an initial minimum set of requirements for inclusion in a
maintenance program at aircraft entry into service with the operator. The analysis of feedback from
service may subsequently justify changes to these requirements in order to maintain program
effectiveness.
Development of the MPD is part of the Scheduled Maintenance Process, itself identified in the Airbus
DOA (Design Organisation Approval) and is audited on a regular basis in the frame of the Airbus
Quality Assurance System. As such, the MPD complies with the content of several approved source
documents.
NOTE: Compliance with the MPD does not automatically imply compliance with the minimum set
of scheduled maintenance requirements that shall be observed. Especially for mandated
requirements originating from ADs and ALS Parts, operators are advised to check
independently from the information in the MPD, that these requirements are covered by
their Maintenance Program.
B. COVERAGE
This A330 MPD Revision contains tasks from the following source documents:
A330 MRBR (Maintenance Review Board Report) Revision 20.
ALS Part 2 Damage Tolerant Airworthiness Limitation Items (DT-ALI), Revision 04.
ALS Part 3 Certification Maintenance Requirements (CMR), Revision 07.
ALS Part 4 System Equipment Maintenance Requirements (SEMR), Revision 08.
ALS Part 5 Fuel Airworthiness Limitations (FAL), Revision 04.
ETOPS, Configuration, Maintenance, Procedure (CMP) document Revision 34.
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NOTE: The simplified MPD concept retains some Engine Manufacturer VSB related tasks from
Rev 23. Since these have not been addressed by Airbus source documents, further
assessment will be made to determine whether any should be given ICA status (and
included in the MRB Report) before they are removed.
The information and instructions included herein are applicable to the following A330 models and
powerplants. They are valid for use on an in-service aircraft only if the model is listed in the TypeCertificate Data Sheet:
A330-20x with GE CF6–80E engines
A330-22x with PW 4000 engines
A330-24x with TRENT 700 engines
A330-30x with GE CF6–80E
A330-32x with PW 4000 engines
A330-34x with TRENT 700 engines
A330-20xF with GE CF6-80E engines
A330-22xF with PW 4000 engines
A330-24xF with TRENT 700 engines
A330-84x with TRENT 7000 engines
A330-94x with TRENT 7000 engines
The third digit of the hyphenated number is identified as "x" in order to indicate that all aircraft models
in this series are covered by this MPD. The final digit in the official aircraft designation is associated
with thrust levels and has no repercussion on the MPD.
For further clarification, the following table provides an example of the specific aircraft models
included in the above-mentioned designations. The right hand list in this table may not be exhaustive.
Generic model designation
Specific model designations
A330-20x
A330-22x
A330-24x
A330-30x
A330-32x
A330-34x
A330-20xF
A330-22xF
A330-24xF
A330-84x
A330-94x
A330-201, A330-202, A330-203
A330-223
A330-243
A330-301, A330-302, A330-303
A330-321, A330-322, A330-323
A330-341, A330-342, A330-343
A330-200F
A330-220F
A330-240F
A330-841
A330-941
NOTE: Within the MPD the Applicability of individual tasks is, where necessary, defined using
generic series i.e. A330–200, A330–200F, A330–300, A330–800, A330–900.
Included in this MPD are maintenance tasks for the following Auxiliary Power Units (APU):
-
GARRETT GTCP 331-350 (c)
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C. SCOPE/LIMITS OF THE MPD SOURCE DOCUMENTS
The information and instructions included herein are only applicable to parts installed through an
Airbus modification / service bulletin and are not intended to cover parts installed through a
Supplemental Type Certificate (STC).
The tasks and frequencies in this MPD have been developed and are valid for aircraft in operation. If
an aircraft is not in operation e.g. parked or stored, the instructions quoted in AMM chapter 10 should
be followed.
The tasks in this MPD are based on various source documents, each having its own scope/limits.
-
MRBR tasks:
The A330 MRB Report is based on an aircraft utilization of between 1667 FH to 5667 FH or from
367 FC to 2200 FC within a 12 month period. Operators whose aircraft utilization differs from
these parameters may need to make adjustments to their customized scheduled maintenance
program together with their regulatory authority.
Details are provided in OIT reference: 999.0002/21 Rev 00 dated 01-MAR-2021
-
ALS Part 2: Damage Tolerant Airworthiness Limitation Items (DT-ALI) tasks:
The airworthiness limitations from ALS Part 2 allow operation defined by the Maintenance
Program Publication Trigger (MPPT). Refer to the introduction of the ALS Part 2 (ALI).
-
ALS Part 3 (CMR) tasks:
The CMR limitations allow operation defined by the Maintenance Program Publication Trigger
(MPPT). Refer to the introduction of the ALS Part 3 (CMR).
-
ALS Part 4: System Equipment Maintenance Requirements (SEMR) tasks:
The SEMR limitations allow operation defined by the Maintenance Program Publication Trigger
(MPPT). Refer to the introduction of the ALS Part 4 (SEMR).
ALS Part 5: Fuel Airworthiness Limitations (FAL) tasks:
The FAL limitations allow operation defined by the Maintenance Program Publication Trigger
(MPPT). Refer to the introduction of the ALS Part 5 (FAL).
-
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2. REVISIONS
The A330 MPD is revised to reflect:
–
–
–
Revisions of source documents
Updated AMM procedure references
Updates of data not contained in the source documents
MPD Revisions are launched to reflect revisions to the ALS and/or MRBR such that, as far as possible,
publication of impacted documents is synchronized.
Data control instructions for each MPD revision are provided in the Summary Of Changes (SOC). Prior to
incorporating a revision, the operator shall ensure that the previous revision has been incorporated.
In between MPD Revisions, updates of the MPD, called “MPD Revision Information” are available on
AirbusWorld in the following location:
-
AirbusWorld > Content library > Maintenance and Engineering > Scheduled Maintenance
Requirements > MPD Information
For detailed information refer to the introduction of the MPD Revision Information
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3. IMPLEMENTATION AND ACCOMPLISHMENT OF NEW / REVISED TASKS
A. GENERAL
Instructions for the introduction of new or revised recommendations into an existing maintenance
program are typically established by the operator’s National Aviation Authority.
This paragraph is included in the MPD to provide guidance to an operator who may not have locally
approved instructions concerning:
-
how to introduce new or modified tasks into an existing maintenance program, or
how to schedule the accomplishment of such tasks on aircraft for which the recommendation is, or
soon will be, overdue.
It is not intended that operators seek to change existing NAA instructions based on these
recommendations.
The simplified MPD content introduced in 2017 resulted in the removal of:
-
tasks that had been introduced to reflect Airworthiness Directives (AD) and
Airbus recommendations not identified as Instructions for Continued Airworthiness such as
Inspection Service Bulletins (ISB) and Service Information Letters / In-Service Information articles
(SIL/ISI).
The guidance provided in this paragraph is now limited to new and modified requirements that reflect
changes introduced in the Airworthiness Limitation Section (ALS), the MRB Report or the ETOPS
Configuration, Maintenance and Procedures (CMP) document.
It is reminded that the MPD is not a source document for any maintenance recommendation. The
start date for determining the Implementation Period and the Compliance Time is the publication date
(or, if quoted, the effective date) of the source document, not the MPD.
B. DEFINITIONS
The terms that describe the time periods associated with introduction of new recommendations are
not always clearly defined in regulatory documentation and are not necessarily harmonised between
different countries. For the purposes of the Airbus MPD guidance material the following definitions
are used.
1. Implementation Period:
The period of time between the publication date (or, if quoted, the effective date) of a new or
revised recommendation in a source document and the introduction of that recommendation in the
operator’s approved maintenance program.
2. Compliance Time:
The period of time given to operators to accomplish maintenance tasks and/or replace items (at
component or aircraft level) having exceeded, or close to exceed, the new or reduced interval
provided in the source document.
C. GUIDANCE ACCORDING TO SOURCE OF MPD TASK
Unless advised otherwise in the transmittal details, new and revised requirements should be
implemented into the operator’s maintenance program within 12 months of the publication date, as
far as is practicable.
The following paragraphs address Compliance Time for tasks originating from the various MPD
source documents.
1. Damage Tolerant - Airworthiness Limitations Items (DT-ALIs) – ALS Part 2
Airbus target publication of DT-ALIs at least two years before they become due on the first
aircraft. In cases where this two year period is not achieved, it is recognized that it may be difficult
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(or impossible) to schedule the task on a particular airframe before it comes due. In such cases,
Airbus will review the particular utilization and type of operation to determine if an alternate means
of compliance can be developed.
Airbus is not normally able to issue a generic compliance time for DT-ALIs. DT-ALI compliance
periods must be handled on a case by case basis, using specific utilization data from concerned
aircraft. Operators should ensure they do not exceed the limitation without prior agreement with
the manufacturer, the local airworthiness authority and the certificating authority. In exceptional
circumstances a DT-ALI may be issued which is already overdue or close to be overdue on a
particular aircraft. In such cases the ALS Part 2 transmittal details will advise an appropriate
compliance time for first time accomplishment on aircraft where the task is already overdue or will
become overdue within the quoted threshold / interval. Operators may also contact Airbus for
specific advice.
2. Certification Maintenance Requirements (CMRs) – ALS Part 3
New requirements in ALS Part 3 revisions should only result from the certification of design
changes and thus are normally published before the subject design feature enters service. If for
any reason a CMR becomes valid on a design configuration already in service then the ALS Part
3 transmittal details will advise an appropriate compliance time for first time accomplishment on
aircraft where the task is already overdue or will become overdue within the quoted threshold /
interval.
3. System Equipment Maintenance Requirements (SEMR) (previously referred to as Ageing
Systems Maintenance (ASM)) – ALS Part 4
The ALS Part 4 transmittal details will advise an appropriate compliance time for first time
accomplishment on aircraft where the task is already overdue or will become overdue within the
quoted threshold / interval.
4. Fuel Airworthiness Limitation Items (FAL) – ALS Part 5
The ALS Part 5 transmittal details will advise an appropriate compliance time for first time
accomplishment on aircraft where the task is already overdue or will become overdue within the
quoted threshold / interval.
5. MRB Report and MRB Report Temporary Revision (TR)
MRB Report (MRBR) tasks arise from a theoretical analysis of the aircraft prior to entry into
service. Tasks from the Systems and Powerplant Section are categorized according to whether
they are associated with hidden or evident conditions and according to their contribution to the
avoidance of safety and non-safety related failure effects. These categories (Failure Effect
Categories – FECs) give an idea of 'importance' or 'criticality' (FEC 5, 8, 9, 6 and 7 in decreasing
order of importance) and allow a different compliance time policy to be established for different
categories.
The MRBR is a report containing the initial minimum scheduled maintenance/inspection
requirements for derivative or newly type certificated transport category aircraft. Operators of the
aircraft type should implement the MRBR or revisions thereto, in accordance with established
procedures. It should be noted that the MRBR is not the aircraft maintenance program but does
provide the initial basis for such a program. Depending on an operator's capabilities and overall
maintenance experience, adjustments to initial maintenance program tasks and intervals may be
approved by the operator's National Aviation Authority.
National regulations vary as to how an operator controls his program after entry into service.
Typically, a Reliability Control Program (RCP) will be developed that will identify changes
necessary to maintain an acceptable level of continued airworthiness, operational capability and
economic operation. Some operators may move off the MRBR and rely entirely on their RCP
together with Airworthiness Directives, the ALS amendments and, sometimes, Service Bulletins.
According to NAA regulations, operators are typically required to assess all new
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recommendations made in revisions to MRB Reports. Though Airbus expects operators to reflect
all applicable tasks in their programs there is no requirement for this and an operator may have
justification to substantiate that the task is not effective in their operation.
When a new requirement is identified for inclusion in the Maintenance Program, the operator will
normally use engineering judgment to determine when the task should be accomplished for the
first time, or when a revised task should be next applied after an interval change. The reason for
the revised requirement will normally be evident and thus an assessment of the relative risk and
impact caused by delayed accomplishment can be made.
In the absence of locally agreed policy, Airbus suggests the following guidelines:
– For Systems/APU/Powerplant tasks, non-ALI and non-CPCP related Structure tasks and
ZIP tasks
For new or revised task requirements that are already overdue or will become overdue within the
quoted threshold / interval, perform the task in the next scheduled check package when the
aircraft is on ground long enough to accomplish the task and any necessary corrective actions.
This might not be the next check (for which the planning may be completed) but it would be
expected in the following one if ground time is appropriate.
If task elapsed time is short and any possible corrective action is easily addressed, operators
should consider first performance of at least the FEC 5 and 8 tasks at the next convenient block
A-check (or equivalent) or during the next check opportunity if an equalised program is used.
Unless stated otherwise in information provided at time of MRB Report / Temporary Revision
publication, if the required access is not normally scheduled until the intermediate (6 YE) or heavy
maintenance check (12 YE), e.g. tasks requiring fuel tank entry or galley / lavatory removal,
Airbus recommends accomplishment no later than the next due interval. Overdue FEC 5 & 8 tasks
should be accomplished no later than the next intermediate (6 YE) maintenance check.
– For CPCP related tasks
A new or revised CPCP requirement is normally associated with corrosion findings. In the case
where the task is overdue or will be within the due interval, the operator needs to consider his
local operating conditions in order to assess the potential for corrosion in this area on his
particular aircraft. It is recommended to perform the task as soon as possible on at least one
aircraft in the fleet in order to help make this assessment. Delay in accomplishment may lead to
higher repair costs but not a loss of continued airworthiness. Note that if a safety concern exists, a
new CPCP task recommendation on an in-service aircraft would be promulgated by ISB (and
possibly AD) in addition to inclusion in the MRB Report.
– For ATA 20 tasks related to EWIS or L/HIRF
For new or revised task requirements that are already overdue, or will become overdue within the
quoted threshold / interval, perform the task at the operator's next convenient hangar
maintenance opportunity (typically C-check or equivalent) unless access is assessed as
insufficient to perform the task without exceeding the scheduled out-of-service period. If that is the
case, the task should be performed at the next access opportunity (e.g. at the intermediate (6YE)
or heavy maintenance check (12 YE)) but not exceeding the task interval counting from
publication of the requirement.
6. Fatigue Monitoring Program (FMP)
For a new or revised FMP requirement that is already overdue for a particular aircraft, the
performance of the new task should be planned at the next Heavy Maintenance Visit (HMV) of
that aircraft (multiple of 6 YE or equivalent operator’s HMV (e.g. 84 MO) approved by their NAA).
If the time between publication of the new FMP requirement and the next HMV for an aircraft is
considered insufficient in consideration of the time required for implementation in the operator’s
maintenance program and the check planning, the subsequent HMV can be selected for the first
application of the new FMP requirement.
Example: An aircraft is 17 YE old when a new 12 YE FMP inspection requirement is published. If
it is not feasible that the FMP inspection requirement can be performed during the upcoming 18
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YE HMV, the FMP inspection requirement should be performed during the subsequent HMV (24
YE equivalent HMV).
Airbus recommends to perform all FMP inspection requirements in the frame of the Heavy
Maintenance Visit (HMV).
For NOTE A FMP tasks:
In the case an aircraft in an operator’s fleet reaches the repeat interval (e.g. 18 YE) before the
initial threshold (e.g.12 YE) has been adjusted, then the FMP inspection should still be
accomplished at the repeat interval for that particular aircraft. This repeat accomplishment would
not count twice towards the contribution of the FMP requirement fulfilment for the initial threshold
inspection (e.g. 12 YE), but would count once towards the contribution for the initial threshold (e.g.
12 YE) and once towards the adjusted threshold (e.g. 18 YE).
For NOTE B FMP tasks:
In the case an operator has already accomplished 10 or more inspections at or above the ALS
Part 2 Threshold, the NOTE B FMP task can be deleted from its maintenance program.
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4. INTERVAL/THRESHOLD CONVENTIONS
A. GENERAL
All task intervals are expressed in terms of usage parameters, i.e. FH, FC or calendar time (years,
months, days).
The basic initial inspection check intervals stated below.
The C and 2C letter check intervals have been cancelled in MRBR rev 13 and replaced with intervals
stated in terms of usage parameters, FH, FC or calendar time (years, months). However, since it was
considered important to have “guidance” intervals, target values were used when defining appropriate
intervals. These values were used by the Working Groups during the maintenance task development
as a guideline:
Systems, APU and Power Plant Section
The ‘A’ and multiple ‘A’ letter check intervals have been cancelled in MRBR rev 19 and replaced with
intervals stated in usage parameter (FH).
•
For former A-Check interval the equivalent interval values
are:
1000 FH and multiples
•
For the former C Check interval the equivalent interval values
are:
24 MO or 12000 FH
•
For the former 2C Check interval the equivalent interval
values are:
48 MO or 24000 FH
•
4C-Check
6 Years
•
For the former 8C Check interval, the equivalent interval
value is:
144 MO
NOTE: Some former C and 2C check interval tasks will have more than one parameter stated.
The above intervals were not achieved for all tasks, so some tasks have lower values.
NOTE: The 4C letter check interval still exists in MRBR rev 19 but a significant number of 4 C
task intervals have been converted to 72 MO.
The ‘8C’ letter check intervals have been cancelled in MRBR rev 19 and rev 20, and replaced with
intervals stated in calendar time (months).
For safety related tasks, intervals are given in the appropriate usage parameter (e.g. flight hours,
flight cycles, calendar time). For non-safety tasks, intervals may be quoted in terms of letter check
unless degradation is predominantly dependent on a particular usage parameter or in service
experience did not support escalation.
Structure Section:
For the Structure section, the basic initial thresholds and intervals for environmental deterioration
related items are as follows:
Thresholds:
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Intervals:
6 Years and 12 Years
NOTE: Some calendar thresholds and intervals remain at 5 Years or 10 Years, pending further
evolution.
Thresholds and intervals for fatigue damage related items are given in Flight Cycles (and Flight
Hours for range sensitive items).
Zonal Section:
The ‘A’ and multiple ‘A’ letter check intervals have been cancelled in MRBR rev 19 and replaced with
intervals stated in calendar time (MO).
The ‘4C’ letter check intervals have been cancelled in MRBR rev 19 and replaced with intervals
stated in calendar time (months).
The ‘8C’ letter check intervals have been cancelled in MRBR rev 19 and replaced with intervals
stated in calendar time (months).
•
For the former A Check interval the equivalent interval values
are:
6 MO and multiples
•
For the former C Check interval the equivalent interval value
is:
24 MO
•
For the former 2C Check interval the equivalent interval
value is:
48 MO
NOTE: The above intervals were not achieved for all tasks,
so some tasks have lower values.
•
For the former 4C Check interval the equivalent interval
value is:
72 MO
•
For the former 8C Check interval the equivalent interval
value is:
144 MO
The MPD is not intended to be the total maintenance program. There are items that are typically
performed by each operator in his maintenance program more frequent than 1000 FH / 6 MO. The
routine content of checks occurring more frequently than 1000 FH / 6 MO shall be developed by the
operator and approved/accepted by their local Regulatory Authority. Maintenance/inspection tasks
with intervals more frequent than 1000 FH / 6 MO found in this MPD were developed through the
MSG-3 analysis process.
An operator may desire to perform letter check interval tasks as part of a continuous or a progressive
maintenance program system, i.e. letter check interval tasks would be phased into a number of
individual packages. This would be considered acceptable provided the maximum interval between
successive tasks does not exceed that listed in this MPD.
NOTE: The 4C letter check definitions are based on the original “C” letter check interval value of
18 months. If a higher interval value is used for the “C“ interval , operators must ensure
that the 4C intervals do not exceed 72 MO, unless the increase has been agreed by a
local airworthiness authority.
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B. INTERVAL/THRESHOLD PARAMETERS
The following interval parameters are used in this MPD:
Operational units (usage parameters)
–"FH" (Flight hours)
:
Elapsed time between wheel lift off and touchdown.
–"FC" (Flight cycle)
:
A complete take off and landing sequence.
–“CRR FH” (Crew Rest Room
Flight Hours)
:
CRR operating flight hours
Calendar units
–"HR" (Hour)
:
One Calendar hour elapsed.
–"DY" (Day)
:
24 Calendar hours elapsed.
NOTE: “DY” interval may be counted from 00:00 o'clock of next
day (has not to include remaining day time since task
completion).
–"MO" (Month)
:
One Calendar month.(can be calculated as 1/12 calendar year).
E.g.: Task with 9 MO interval is performed 12 July 2014. The next
due date is then 11 April 2015 23:59.
– "YE" (Year)
:
One Calendar year (can be calculated as 365.25 days).
E.g.: Task with 6YE interval is performed 12 July 2014. The next
due date is then 11 July 2020 23:59.
– CRR MO” (Crew Rest
Room Month)
:
CRR operating months
Other codes
–
"NOTE”
Refer to the note in the task description.
C. GENERAL INTERVAL/THRESHOLD RULES
– When intervals or thresholds with different units (parameters) are assigned to a task, the
interval/threshold expiring first shall apply, if not otherwise stated.
– Task interval parameters expressed in this MPD may be converted to an individual operator's
desired unit (flight hours, cycles or calender time), provided this conversion does not result in the
operator exceeding the initial requirements reflected in the MPD.
– The thresholds and intervals quoted in calendar time in this document include aircraft time in and
out of service.
In other words, operators will not, in general, be allowed to take credit for time out of service or
storage periods to extend calendar inspection thresholds/intervals. Exceptions to this can be
considered by Airbus Maintenance Engineering but will depend on variables such as time
duration, aircraft age, environment and where aircraft was in maintenance cycle.
Specific advice can be given by Airbus Maintenance Engineering on a case-by-case basis if
relevant aircraft details are provided.
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–
Intervals of tasks with source “MRBR” may be changed in accordance with operator's Regulatory
Authority practices and rules. In this respect, attention is drawn to the task origin and the
following:
for Systems and Powerplant tasks, to the Failure Effect Category (FEC) noted in Section C
of MRBR and reflected in “SOURCE” column of this MPD.
for Zonal tasks, to the frequency of the General Visual Inspection tasks transferred from
Structures or Systems and Powerplants.
for ATA chapter 20 not to delete tasks with the identifier “EWIS” or L/HIRF from the
operator's maintenance program.
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5. MAINTENANCE CLOCK STARTING POINT
Unless otherwise specified by AIRBUS in the documentation of an aircraft at time of first delivery, the
starting point for calculation of the due dates or times of all aircraft maintenance tasks is identified in the
following paragraphs.
The Transfer of Title (ToT) is when conformity and contractual documentation is handed over and the
Certificate of Acceptance is signed, this identifying the official transfer of ownership to the first buyer. In
the absence of the date of ToT, an operator may refer to the ‘Delivery Date’ as recorded in the In-Service
Data ‘Aircraft History’ file available on Airbus|World.
A. General rule
The date of first (ToT) may be used as the starting point for the following:
•
•
•
Systems / Power Plant tasks with intervals expressed in airframe FH, FC or Calendar Time
(except as identified in paragraph “B. Specific guidance”)
Structure tasks with an interval quoted in Calendar Time
Zonal tasks
NOTE: This may not be valid if the first ToT occurs more than 90 days after first flight. In this
situation specific guidance on when the clock starts may be given to the operator at time
of delivery. If no record exists that this information was provided, or if details are not
available, then, with the exception of the landing gear TBO, any task that has not yet been
accomplished shall be conservatively planned with reference to first flight date plus 90
days. Exceptionally, for the landing gear TBO, the task may be planned with reference to
first flight date plus 180 days.
First flight shall be used for all structure tasks with an interval quoted in FH, FC or LDGS.
Tasks with intervals quoted in terms of component FH or component FC (e.g. APU Hours, Engine
Cycles, ACT FH) shall be counted from First Flight of the component.
NOTE: For tasks with thresholds / intervals expressed in multiple parameters, the due date is the
earliest determined in consideration of the clock starting point for each parameter
considered individually. E.g. a structure task with threshold 12 YE or 30000 FC or 60000
FH shall be performed within 12 YE of first Transfer of Title or 30000 FC of first flight or
60000 FH of first flight, whichever is reached first.
For repeat maintenance tasks, the interval is counted from the time the maintenance task was
previously performed.
The time to start the clock for Systems & Power Plant tasks and Zonal with applicability determined
by post-delivery modification embodiment is the date of embodiment. For Structure tasks with
applicability determined by post-delivery modification embodiment, refer to dedicated notes in the
section introduction or the task description for determination of clock starting time.
B. Specific guidance
– For ALS Part 2 (DT-ALI) tasks:
•
The threshold is the time at which the maintenance task is first due.
- Threshold limitations quoted in FC or FH count from first flight.
- Threshold limitations quoted in Calendar Time may be counted from the Transfer of Title to the
first operator.
•
In cases where the first task is accomplished very early, the next task can be performed at
the threshold (rather than the repeat interval).
•
When alternative inspection methods are provided, the next interval applicable is the one
associated with the inspection method used at the previous inspection.
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–
–
–
–
–
–
•
"Touch and Go" cycles can be neglected if they are less than 5% of the total number of
Flight Cycles up to threshold inspection or between two consecutive inspections. Each "Touch
and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold inspection or
between two consecutive inspections.
For ALS Part 3 (CMR) tasks:
•
Limitations quoted in FH or Calendar Time may be counted from the Transfer of Title to the
first Operator.
This policy is agreed with EASA in consideration of the very low number of FH performed between
first flight and delivery, and the methodology used to define the value of CMR task limitations.
•
Limitations quoted in FC count from first flight.
For ALS Part 4 (SEMR) tasks (previously referred to as ASM):
•
Limitations controlled at aircraft level and quoted in Calendar Time count from the Transfer
of Title to the first operator.
•
Limitations controlled at aircraft level and quoted in FH, FC or LDGS count from first flight.
•
Limitations controlled at component/subassembly level and quoted in Calendar Time, FH,
FC or LDGS count from the date at which the component/item accomplishes the first flight for
which it will undertake its intended function.
For ALS Part 5 (FAL) tasks:
•
Limitations quoted in FH or Calendar Time may be counted from the Transfer of Title to the
first operator. This policy is agreed with EASA in consideration of the very low number of FH
performed between first flight and delivery, and the methodology used to define the value of FAL
task limitations.
•
Limitations quoted in FC count from first flight.
For an overhauled landing gear or a new landing gear installed after first Transfer of Title:
the start date for Calendar Time tasks is the date of the gear’s first flight after installation. If this
first flight takes place more than 90 days after installation contact Airbus Maintenance Programs
Engineering using TechRequest on-line tool. For the original LDG, paragraph ‘1. General Rule’
applies.
For equipment having intervals defined by National Requirements (NR) or annotated with a
NOTE that requires the task to be managed according to component service history, the
starting point is the date of manufacture or previous task accomplishment on the component or
the first flight for which it will undertake its intended function (for FH and FC tasks) unless
otherwise stated by vendor or National Authority.
If the date of manufacture refers only to the month then, for the purposes of scheduled
maintenance planning, the subsequent maintenance actions can be scheduled with reference to
the last day of that month.
For components addressed by Airworthiness Directive (AD): as stated in the AD.
Summary:
Source
MRBR
ALS
ISSUE: JUL 01/21
Calendar Time
Flight Hours
Flight Cycles
or Landings
SYSTEM
TOT
TOT
TOT
STRUCTURE
TOT
1st Flight
1st Flight
ZONAL
TOT
TOT
TOT
Part 1 (Life
Limitations)
1st Flight
1st Flight
1st Flight
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Source
Calendar Time
Flight Hours
Flight Cycles
or Landings
Part 2
TOT
1st Flight
1st Flight
Part 3
TOT
TOT
1st Flight
Part 4 (aircraft level)
TOT
1st Flight
1st Flight
Part 4 (component
level)
1st Flight
1st Flight
1st Flight
Part 5 Section 3 (Life
Limitations)
1st Flight
1st Flight
1st Flight
Part 5 Section 4
TOT
TOT
1st Flight
New or overhauled LDG installed after
first ToT
1st Flight after
installation*
N/A
1st Flight after
installation
NR, VR or Note requiring task to be
managed according to component
service history
Date of
Manufacture or
date of previous
task
accomplishment
on the
component**
Date of
Manufacture or
date of previous
task
accomplishment
on the
component**
Date of
Manufacture or
date of previous
task
accomplishment
on the
component**
AD
See AD
See AD
See AD
* Contact Airbus if first flight takes place more than 90 days after installation
** Unless otherwise stated in vendor or National Authority documentation
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6. INTERVAL ESCALATION
A. MRBR tasks
The individual task intervals shown in this MRBR may be adjusted with approval from the operator’s
appropriate Regulatory Authority. If a task is escalated, it must be based on satisfactory
substantiation by the operator and review and approval by its appropriate Regulatory Authority, or in
accordance with the operator’s Reliability Program which has been approved by the appropriate
Regulatory Authority. However, tasks with Failure Effect Category (FEC) 5 and 8 must not be deleted
from the operator's maintenance program. Furthermore, ATA 20 tasks must not be deleted (these are
L/HIRF and EZAP tasks for which there is no FEC
–
–
For Operators under U.S. FAA Jurisdiction only:
Operators requesting revisions to the baseline EWIS task or description must submit their request
through the cognizant Flight Standards District Office, who may add comments and then forward it
to the manager of the appropriate FAA Aircraft Certification Office, or office of the Transport
aircraft Directorate, having cognizance over the type certificate for the affected aircraft for
concurrence prior to approval. Task intervals may be revised through normal operator approval
process.
Tasks indicated with “(EWIS)” after the task description must not be deleted from the operator's
maintenance program.
For Operators Not under U.S. FAA Jurisdiction:
Operators requesting revisions to the EWIS requirements may revise these tasks and intervals
through their normal operator approval process. Tasks indicated with “(EWIS)” after the task
description must not be deleted from the operator's maintenance program.
B. ALS Part 2 (DT-ALI) tasks:
Threshold and intervals of the DT ALIs cannot be increased, unless advised by the manufacturer
following approval by the Authority of the State of aircraft registry.
C. ALS Part 3 (CMR) tasks:
Certification Maintenance Requirements (CMR) tasks generated by systems safety assessment shall
not be deleted from an operator's maintenance program.
–
–
CMR*:
One Star CMRs specified in the ALS Part 3 are mandatory tasks and cannot be changed or
deleted without the concurrence of the Primary Certification Authority (EASA). One Star CMR task
intervals quoted in ALS Part 3 are absolute limitations and cannot be escalated without the
concurrence of the Primary Certification Authority (EASA).
CMR**:
Two Star CMRs specified in the ALS Part 3 are mandatory tasks and cannot be changed or
deleted without the concurrence of the Primary Certification Authority (EASA). Two Star CMR task
intervals may be adjusted in accordance with an Operator's approved escalation practices or an
approved reliability program, but the task content may not be changed or deleted without prior
Primary Certification Authority (EASA) approval.
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7. PERMITTED VARIATIONS TO MAINTENANCE PERIODS
(alternatively referred to as Short-Term Extension or Short-Term Escalation)
A. GENERAL
A permitted variation should normally be granted by the National Aviation Authority (NAA), unless
that Authority has agreed to delegate such possibility to the operator. A permitted variation to a
period required by the maintenance programme may be granted by the Authority on a case-by-case
basis on occasions where the operator does not have the ability to perform the required maintenance
within the prescribed interval. Contrary to an amendment to the Maintenance Programme, a
permitted variation applies to a unique aircraft, for a unique occasion
A permitted variation should not be understood to be a maintenance planning tool, but as an
exceptional means to allow the operator to fly for a limited period of time until the required
maintenance is performed. The use of this provision should be limited to occasions when compliance
with the approved maintenance programme cannot be achieved due to circumstances which could
not reasonably have been foreseen by the operator. Typical reasons could include:
-
failure of the ground support equipment required to perform the task or
non-availability of a hangar due to late release of another aircraft or
significant ground damage event on another aircraft in the fleet, or
failure of an external provider to deliver according to agreed schedule.
It is normal practice for an operator to include the permitted variation policy in their Continuing
Airworthiness Management Exposition, Continuous Airworthiness Maintenance Program (CAMP) or
equivalent. The details of this will be determined in conjunction with the operator’s NAA.
The text in the paragraph below titled MAXIMUM VARIATIONS constitutes an Airbus
recommendation that may be useful to operators in the absence of NAA guidelines on the subject.
These are based on Temporary Guidance Leaflet (TGL) N° 26 formerly established by JAA. EASA
subsequently determined that the use of Variations is an operational issue and thus the responsibility
for issuing such guidelines is that of the NAA. As a result, the JAA document was cancelled and can
no longer be quoted as a reference.
Examples of National guidelines include CAA (UK)’s CAP 562 Book 2, Leaflet 5-30 paragraph 6 &
Appendix A and FAA’s Flight Standards Information Management System (FSIMS) Order 8900.1
Volume 3 Chapter 37 Section 1.
The policy related to permitted variations does not apply to all maintenance tasks. The list of
prohibitions may vary according to NAA guidelines. In the absence of local guidance, the following
should be considered as excluded:
1. Life limitations identified in the ALS Parts 1, 4 and 5.
2. Tasks required to satisfy Airworthiness Directives related to a specific unsafe condition.
3. Damage -Tolerant Airworthiness Limitation Items as stated in ALS Part 2.
4. Certification Maintenance Requirements, unless specified otherwise in the ALS Part 3 document.
5. Systems Equipment Maintenance Requirements (formerly Aging Systems Maintenance), unless
specified otherwise in the ALS Part 4.
6. Fuel system Airworthiness Limitation Items, unless specified otherwise in the ALS Part 5
document.
7. ETOPS CMP maintenance tasks with intervals quoted as ‘not to exceed’, unless specified
otherwise in the CMP document.
NOTE: Any ETOPS related tasks not excluded by the above can benefit from a permitted variation
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without impacting the ETOPS capability, i.e. ETOPS flights may be conducted while under the
permitted variation.
NOTE: The above list of exclusions does not mean that the Authority cannot permit a deviation of
an AD, Life Limitation etc., but that this paragraph addressing a generic permitted
variations policy does not apply to such tasks.
Variations greater than those detailed in paragraph PERMITTED VARIATIONS TO MAINTENANCE
may be justifiable on a case by case basis taking into account the specific aircraft and its service
history. Operators are invited to contact Airbus Maintenance Programs Engineering (via
TechRequest) to identify the potential for issuance of an Airbus Statement of Airworthiness
Compliance (ASAC) or Airbus Maintenance Program Engineering Statement (AMPES) which, if
feasible and appropriate, may be used to support the operator’s discussion with their local Authority.
Details of the ASAC/AMPES are provided in OIT references:
For ASAC purposes: 999.0086/09 dated 5 October 2009 999.0076/12 dated 3 October 2012.
For AMPES purposes: 999.0069/19 dated 9 October 2019.
B. PERMITTED VARIATIONS TO MAINTENANCE
The maximum variation of a prescribed period is indicated below.
1. Items controlled by flight hours:
(i) 5000 flying hours or less: 10%
(ii) More than 5000 flying hours: 500 flying hours
2. Items controlled by calendar time:
(i) 1 year or less: 10% or 1 month whichever is the lesser
(ii) More than 1 year, but not exceeding 3 years: 2 months
(iii) More than 3 years: 3 months
3. Items controlled by landing/cycles:
(i) 500 landings/cycles or less: 5% or 25 landing/cycles, whichever is the lesser.
(ii) More than 500 landings/cycles: 5% or 250 landings/cycles, whichever is the lesser.
4. Items controlled by more than one limit: For items controlled by more than one limit, e.g. items
controlled by flying hours and calendar time or flying hours and landings/cycles, the more
restrictive limit should be applied.
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8. GENERAL RULES
The following rules, apply to the A330 maintenance program:
A. The operator's manuals shall contain the details and responsibilities for accomplishing the
maintenance identified by this document.
B. The overall reliability of the A330 will be monitored by each operator's system for continuous analysis
and surveillance as required by the operator's Regulatory Authority.
C. Task intervals of tasks with source “MRBR” may be changed in accordance with operator's
Regulatory Authority. However, tasks with Failure Effect Category 5 and 8 must not be deleted from
the operator's maintenance program. In this respect, attention is drawn to the task origin (refer to
MPD “SOURCE” column).
D. Each operator should be aware of the various inspection techniques such as X-Ray, ultrasonic, eddy
current, radio isotope, which are available and described in the Non Destructive Testing Manual
(NTM).
The use of such techniques can be developed to provide a valuable adjunct to the prescribed visual
inspections. For any substitution of such inspection technique, it must be ensured that the same
damage size will be detectable by the proposed technique with, at least, the same level of
confidence.
E. Items that are life limited will be removed from service according to the life limits stated in the
appropriate section of the engine or aircraft manufacturer's manuals. These sections are referenced
in the aircraft "Type Certificate Data Sheet".
F. Tasks coming from any of the ALS parts must not be deleted and should be handled with specific
associated rules, as described in the subject documents. ALS Part 3 Certification Maintenance
Requirements (CMR) tasks have specific rules regarding escalation as follows:
CMR** :
Task interval may be escalated by an operator, in accordance with an approved reliability
program.
CMR* :
Task interval shall not be escalated by an operator.
ETOPS tasks must not be deleted and should be handled according to specific rules described in the
ETOPS CMP document. ‘Not to exceed’ intervals shall not be escalated.
G. Tasks may be considered to conform to the requirements of the scheduled maintenance program if
accomplished as part of a Regulatory Authorities approved/accepted equivalent check/test by flight
crew.
H. It is the responsibility of each operator to adjust his own maintenance program in accordance with his
National Requirements and to comply with existing rules with respect to reporting to his Regulatory
Authority and to the manufacturer events having effects on the continued airworthiness of the aircraft.
I.
Task interval parameters expressed in this MPD may be converted to an individual operator’s desired
unit (flight hours, cycles or calendar time) provided this conversion does not result in the operator
exceeding the initial requirements of the MPD.
J. The maintenance clock does not stop while the aircraft is on ground or in maintenance condition.
Although the aircraft does not collect any FH or FC when being on ground, attention has to be given
to tasks, where the interval is expressed in calendar time (hours, days, month, year). All tasks that
become due while the aircraft is on ground at the time of the maintenance visit have to be performed
prior to return to service. However, there is no need to repeat inspections during the time on ground
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E.g. during a 4 weeks downtime, tasks with interval 8 DY only need to be performed at the end of the
check (for return to service).
K. The thresholds and intervals quoted in calendar time in this document include aircraft time in and out
of service. In other words, operators will not, in general, be allowed to take credit for time out of
service or storage periods to extend calendar inspection thresholds/intervals. Exceptions to this can
be considered by Airbus Maintenance Engineering but will depend on variables such as time duration,
aircraft age, environment and where aircraft was in maintenance cycle. Specific advice can be given
by Airbus Maintenance Engineering on a case-by-case basis if relevant aircraft details are provided.
L. The reapplication of all protective materials (e.g. Temporary Protection Systems (TPS), paints etc.)
Shall be carried out following their removal to perform the inspection/maintenance task.
M. The CMP (ETOPS) document is the authoritative document for mandatory ETOPS Maintenance
Standards. Where maintenance task intervals in the CMP are more restrictive than required in the
MRBR, these overrule those in the MRBR. Where the MRBR task interval is more frequent than
required by the CMP, the MRBR value remains valid until the operator justifies escalation (the CMP
interval acts as an upper limit to the escalation). Maintenance tasks, which become obsolete due to
an authorized configuration change are not applicable.
N. Any fairings, panels, doors or other items which are removed/opened to gain access for maintenance
tasks must also be inspected for general condition with a minimum level of GVI before
reassembly/refitting.
O. Operators shall report any findings to the manufacturer via the inspection reporting system on
AirbusWorld/Maintenance and Engineering/Prepare Maintenance/Optimize maintenance
management/Optimize maintenance program/Report my check records.
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9. TASK DATA DESCRIPTION
Each section opens with an introduction.
Presentation of maintenance tasks (PDF version)
A common form (except Threshold/Interval for range sensitive tasks) is used for Systems/APU/Power
Plant, Structure and Zonal sections and provides the following information:
A. Revision Code
All new, revised or deleted tasks are given revision codes, in comparison to the previous revision:
•
•
•
N = New
R = Revised
D = Deleted
B. Section
The Section identifier consists of the following parts:
1. Section Number
2. (i) the first two digits of the ATA chapter for systems and powerplant as well as structure tasks
3. (ii) ''ZL” + the main zone identifier for zonal tasks
C. Task number
Each task is identified by a specific MPD task number. When a task applies to two specific main
zones located symmetrically to either side of the aircraft centerline, the task is assigned a single task
number, but both LH and RH zones are indicated in "ZONE" column.
The task number comprises 9 or 10 digits organized as follows :
* ATA reference or zone
*
– Systems, APU and Power Plant
section:
The ATA reference identifies the system/sub system or
component on which the task is to be accomplished.
– Structure section:
The ATA reference identifies the structural significant item on
which the task is to be accomplished (reference identical to
that used in the MRB report).
– Zonal section:
The zone number is preceded by the letter code "ZL". For task
to be repeated in several main zones, the first main zone or
LH zone number is used (aircraft zoning is provided in
customized AMM Chapter 06).
Sequence number
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–
–
Apart from a few cases, the sequence number is used to discriminate between different tasks
relating to the same hardware.
In Section 2 on APU and Power Plant related tasks, the first digit identifies the APU/engine type
concerned:
•“0” for GTCP 331-350 C
•“G” for General Electric
•“P” for Pratt & Whitney
•“R” for Rolls Royce Trent 700
•“N” for Rolls Royce Trent 7000
*
Applicability index
–
The applicability index identifies successive developments of a task, introduced by modifications
or specific requirement. However, in a few cases, the sequence number may be used for that
purpose, when referenced documentation requires to do so.
The technical status or specific requirement associated with each applicability index is specified in
the applicability column. As a general rule, tasks with the same first 8 digits in task number, have
same work description in the AMM.
D. Zone column
The 'Zone' column shows the position(s) where the task has to be accomplished (repeated)
according to the description. Quoting several positions means that the task has to be repeated in
each zone.
Each position is identified by one zone number or one sub-major zone number or one major zone
number.
When a major zone (e.g. 100) or sub-major zone (e.g. 140) or specific zone (e.g. 141) number is
quoted to identify a unique position of a task, the more precise zone numbers are quoted in the
description in case such an additional information is estimated useful.
E. Description column
This column provides the following information:
*
Task title
Identifies the system/sub system/component/zone/structural significant item concerned by the task.
*
Task description
Gives a concise description of the work to be performed.
*
Task preparation (where applicable)
Specifies the preliminary steps (from a pre-established list) to be performed prior the maintenance
task itself.
*
Access (where applicable)
Specifies the identifiers of the access panels, linings or doors to be opened or removed for
accomplishment of the task.
Floor panels of passenger cabin and cargo holds are not designated by their identifiers but by the
frame numbers between which the floor panels have to be removed are quoted.
*
Task code
Specifies the type of task to be carried out
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*
TASK
CODE
DEFINITION
TASK
CODE
DEFINITION
CHK
Check for condition, leaks, circuit
continuity,
Check fluid reserve on item,
Check tension and pointer,
Check fluid level,
Check detector, Check charge
pressure,
Remove and check, Check torque,
Leak Check
OPC
Operational Check
DIS
Discard
RST
Remove for restoration
DET
Detailed Inspection
SDI
Special detailed inspection
FNC
Functional check
SVC
Drain, Servicing, Replenishment
(fluid change)
GVI
General Visual Inspection
VCK
Visual Check
LUB
Lubrication
Skill Code
Specifies the type of skill required for task accomplishment:
SKILL CODE
DEFINITION
SCOPE
AF
AIRFRAME
Hydro-mechanical, environmental, fuel, oxygen
and cargo systems.
Associated servicing requiring a certain
qualification such as:
Flaps/Slats.
Landing Gear.
THS actuator.
Structure Visual Inspection.
•
•
•
•
General cleaning and cleaning prior inspection.
Greasing and oil replenishment not requiring
system knowledge or certain qualification.
AV
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•
•
•
•
•
Autopilot.
Instruments.
Digital equipment.
Fire protection.
Lighting, windscreen ice and rain.
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*
SKILL CODE
DEFINITION
SCOPE
EN
ENGINE
•
•
Engines and APU accessories.
Associated services.
RA
RADIO
•
•
Radio and radio navigation.
Audio interphone, CVR, Pax address.
CA
CABIN
Furnishing, galleys.
EL
ELECTRICAL
Electrical generation, distribution and associated
services.
NDT
NON DESTRUCTIVE
TESTING
All Non-destructive test inspection and
boroscope inspection.
UT
UTILITY
Toilets water, waste water.
TPS (where applicable)
Specifies the type of Temporary Protection System (TPS) to be applied as indicated below:
"1"
:
Type 1 Grade 2 or Grade 3 TPS is to be applied.
"1+2"
:
Type 1 TPS plus a subsequent application of Type 2 TPS is to be applied.
“2”
:
Type 2 TPS is to be applied
“3”
:
Type 3 TPS is to be applied
"No"
:
TPS must not be applied in the area (example: inside fuel tank, pylon).
NOTE: If “1+2” is stated in the TPS column, it is at the discretion of the operator to apply either
“Type 1 TPS plus Type 2 TPS”or“Type 3 TPS”.
If “3” is stated in the TPS column, it is at the discretion of the operator to apply either
“Type 3 TPS”or“Type 1 TPS plus Type 2 TPS.
Specifications for TPS are available in AMM chapter 20-31-00 / Materials list / Storage Preservation.
F. Time Controlled Items (TCI) column
TCI markers are set in order to provide assistance in planning removable assets installed on the A/C.
MPD tasks marked as TCI are connected to the removal/installation of components/parts, which are
to be restored/overhauled/tested in a workshop and then may be re-installed on a different A/C
(rotables).
This does not include components removed, cleaned and put back on the same A/C without going
into a workshop.
The utilisation and selection of TCI is left completely to the discretion of the operator.
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Operator specific TCI selection could e.g. reflect components, which often (or likely) rotate between
A/C due to unscheduled and scheduled replacements.
NOTE: TCI markers are to be seen as a planning help. They are neither demanded by any
source document nor any certification authority.
G. Threshold/interval column
This column provides the following information:
*
100% Inspection Threshold
This information preceded by the letter "T" gives a specific value of an operational parameter or of a
letter code defining the first accomplishment deadline of the task. When threshold is equal to the
interval, the letter "T" may not show.
When the threshold is expressed in several units, the conjunction "OR" separate the different
indications.
*
100% Inspection Interval
This information, preceded by the letter "I", gives a specific value defining the maximum time that can
separate two complete accomplishments of the task.
When the interval is equal to the threshold, the letter "I" may not show.
When the interval is expressed in several units, the conjunction "OR" separates the different
indications.
*
Sample Inspection Threshold
This information, preceded by the letters "ST", gives a specific value of an operational parameter or
of a letter code defining the first accomplishment deadline of the task. When the threshold is equal to
the interval, the letters "ST" may not show.
When the threshold is expressed in several units, the conjunction "OR" separates the different
indications.
*
Sample Inspection Interval
This information, preceded by the letters "SI", gives a specific value of an operational parameter or of
a letter code defining the maximum time that can separate two complete accomplishments of the
task.
When the interval is equal to the threshold, the letters "SI" may not show.
When the interval is expressed in several units, the conjunction "OR" separates the different
indications.
NOTE: Structure section: For task which are range-sensitive:
FH OPTIMIZED:
Threshold/Interval values or Sample Threshold/Sample Interval values (FH optimized
requirements).
FC OPTIMIZED:
Threshold/Interval values or Sample Threshold/Sample Interval values (FC optimized
requirements).
NOTE: EXCEL version (only MPD and 3–STRUCTURES sheet):
NON-RANGE SENSITIVE columns:
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provides Threshold/Interval values or Sample Threshold/Sample Interval values for nonrange sensitive task (FH-OPTIMIZED and FC-OPTIMIZED columns are empty).
FH-OPTIMIZED/FC-OPTIMIZED columns:
provides Threshold/Interval values or Sample Threshold/Sample Interval values for range
sensitive task (NON-RANGE SENSITIVE columns are empty).
H. Source code column
Specifies the source document.
ALI, ALI WFD
:
Task originated by Airworthiness Limitation Section (ALS) Part
2 - Airworthiness Limitation Items arising from fatigue and
damage tolerance evaluation of damage tolerant structural
elements whose failure could contribute to catastrophic failure
of the aircraft (FAR/JAR 25.571) and Airworthiness Limitation
Items arising from an initial evaluation of Widespread Fatigue
Damage.
MRB
:
Task originated from the MRB Report.
For tasks resulting from a system/power plant analysis, the
three letters "MRB" are followed by the corresponding
Functional Failure Effect category (5 – 9).
5 : Evident Safety
6 : Evident Operational
7 : Evident Economic
8 : Hidden Safety
9 : Hidden Non Safety
CMP
:
Task originated by CMP (Configuration Maintenance and
Procedures) . This document lists the standards for ETOPS.
CMR**
:
Task is a Certification Maintenance Requirement (ALS Part
3). Its interval may be changed in accordance with an
approved reliability program. Cannot be deleted from operator
maintenance program.
CMR*
:
Task is a Certification Maintenance Requirement (ALS Part
3). Its interval cannot be escalated by an Operator. Cannot be
deleted from operator maintenance program.
SEMR
:
Task originated by System Equipment Maintenance
Requirements document (ALS Part 4).
FAL
:
Task originated by Fuel Airworthiness Limitations document
(ALS Part 5).
FMP
:
Task that contributes to the Fatigue Monitoring Program. The
Fatigue Monitoring Program (FMP) is defined to indicate
unpredictable early occurrence of fatigue related deterioration
on metallic structure. Tasks are listed in a dedicated non MRB
approved Appendix of the MRB Report.
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CPCP
*
I.
:
Task originating from Corrosion Prevention and Control
Program.
For structure tasks, the type of governing program (100%, CPCP) is indicated in regard with
applicable threshold/interval value.
Reference column
This column provides :
*
*
The AMTOSS reference of the task in the A330 Aircraft Maintenance Manual.
References to technical publications where accomplishment instructions can be found.
*
The MRB reference of the task.
–
MPD tasks in the Systems, APU and Power Plant section provide the MSI reference task number
of the covered MRBR task.
MPD tasks in the Structure section provide the MSI or SSI number of the covered MRBR task.
Nevertheless, they indicate if a zonal task covers the requirements of the SSI inspection (Note: In
this case the zonal task does not cover TPS application).
MPD tasks in the Zonal section provide the MSI number or SSI reference task number of the
covered MRBR task.
–
–
*
*
*
*
The ALI reference of the task in Structure section.
The SEMR reference of the task in Systems, APU and Power Plant section.
The CMR reference of the task in Systems, APU and Power Plant section.
The CMP reference of the task in Systems, APU and Power Plant section.
J. Men — M/H (Manhours) Columns
Task Man-Hours:
This field contains the sum of man-hours required to perform the task per zone. Man-hours only apply
for on-aircraft maintenance. Off-aircraft maintenance, performed in the workshop, is not considered.
NOTE: MPD man-hours are not to be mistaken with elapsed time.
Man-hours are expressed in industrial hours. Where “TBD” is quoted, the man-hours are still to be
defined. Where “N/A” is quoted, man-hours are not applicable, e.g. shop maintenance. For tasks
where different configurations are possible, e.g. in the cabin, the task man-hours based on the
configuration defined in the „Airbus Standard Specification“.
For the calculation of MPD man-hours, the following assumptions apply:
1. The aircraft is in general maintenance condition as described in the AMM.
2. Maintenance personnel is adequately skilled and experienced to perform the task.
3. Airbus recommended equipment is used.
4. Tanks are defueled where tank opening required.
5. Standard safety devices and warning notes are in position.
6. The aircraft is in a clean condition for inspections.
Man-hours quoted in the MPD do not take into account:
1. Non-routine work, e.g. repair, troubleshooting, shop overhaul.
2. Preparatory work such as aircraft cleaning, positioning work stands, connecting ground power
carts.
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MAINTENANCE PLANNING DOCUMENT
3. One-time actions, e.g. de-greasing, stripping, painting.
4. Embodiment of modifications, cabin (galley, lavatory, furnishings) refurbishment.
5. Non-productive time, e.g. shift-change, set-up of tools, waiting for sealant or paint drying.
6. Planning and establishment of procedures.
The task man-hours quoted in the MPD are provided for guidance only and should be adjusted to the
specific operator conditions and efficiency.
Access Man-hours:
This field contains the man-hours for opening and closing of access panels, nacelles and doors.
Either removal/installation or opening/closing is reflected, depending on access panel type. Some
panels may be grouped and quoted as preparations, for easier presentation and planning, especially
among the cabin linings. The number of men for the access work is not given.
Preparation Man-hours:
This field contains the man-hours to perform the preparation for a task. Removal and installation are
included in the preparation man-hours. For preparations where different configurations are possible,
e.g. in the cabin, the preparation man-hours based on the configuration defined in the „Airbus
Standard Specification“. Adjustment of the preparation men-hours to the operators cabin
configuration and optional equipment may be necessary. The number of men for the preparation
work is not given.
Men:
This field contains the minimum number of men necessary to perform the task.
K. Applicability Column
The information given in this column defines the technical status of the aircraft on which the task is
applicable.
The technical status is expressed as one, or a combination, of the following keywords :
*
*
*
*
"ALL" indicates that the task is applicable to all A330 aircraft.
A keyword identifying the aircraft series or model (–200, –200F, –300).
A keyword defining the status with respect to a modification number/service bulletin: PRE 20024
means "before embodiment of modification 20024”.
Keyword "POST ..." means "after embodiment ...".
When applicability is the result of combination of modifications:
POST 20024
OR
POST 23000
==>
means task is applicable for all A/C “POST modification
20024" or all A/C "POST modification 23000".
Applicable to aircraft having:
((MOD))OR((MOD))
PRE 20024
POST 35000
==>
means task is applicable to all A/C “PRE modification 20024
and“POST modification 35000”.
Applicable to aircraft having:
((MOD)AND NOT(MOD))
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PRE 23051
(27–1057)
OR
PRE 23061
(27–1110),
(27–1902)
==>
Task applicable to all A/C WITHOUT modification 23051
(Service Bulletin 27–1057 NOT embodied) and to all A/C
WITHOUT modification 23061 (NEITHER Service Bulletin 27–
1110 NOR Service Bulletin 27–1902 embodied).
Applicable to aircraft having:
(NOT(MOD OR(SB)))OR(NOT(MOD OR(SB)OR(SB)))
When a modification can be retrofitted through an AIRBUS Service Bulletin, the SB number is given
between brackets just below the modification number. A comma between two SB brackets means a
logical “OR” while an “&” between two SB expressions is equivalent to a logical “AND”.
*
*
*
*
*
*
The aircraft Manufacturer Serial Number (MSN) or a block of consecutive serial numbers (e.g.
0005 – 0007 signifies that the task is applicable on aircraft MSN 0005, 0006 and 0007).
”MSN 0050 – 9999” means that the task is applicable on the MSN 0050 and the following MSNs.
A weight variant group expressed, for example "GROUP 32A". This is applicable when a number
of weight variants have a common maintenance requirement. In these cases the weight variants
concerned have been 'grouped together' and classified under a group number, to simplify how the
applicability is stated. The weight variants contained within each weight variant group are listed in
the introduction of the Structure section. Details of individual aircraft weight variants can be
identified by reference to the SRM introduction (Weight Variant Identification List).
A conditional applicability such as “If equipment installed” is selected when a large amount of
modification or combination of modification are applicable to a particular item for a given
equipment.
This avoids stating a complex applicability, which could be confusing and inappropriate for
operators.
e.g. MPD task 256535-02-1 with the applicability “IF ELT INSTALLED”.
The keyword "FAA" indicates that the task is applicable only to aircraft flying under FAA
requirements. The keywords "NON-FAA" indicates that task is applicable for aircraft flying not
under FAA requirements.
Examples:
A330-200
Requirement applicable to -200 PAX series aircraft only.
A330-200F
Requirement applicable to -200 Freighter series aircraft only.
A330-200
OR
A330-300
Requirement applicable to -200 PAX series aircraft or -300
series aircraft.
A330-200
OR
A330-200F
Requirement applicable to -200 PAX series aircraft or -200
Freighter series aircraft.
GROUP 32A
This requirement is applicable to -200 PAX series aircraft with
Weight Variants 020, 021, 022, 023, 024, 025, 026 or 027.
GROUP 32A
PRE 41652
PRE 45749
This requirement is applicable to -200 PAX series aircraft with
Weight Variants 020, 021, 022, 023, 024, 025, 026 or 027, on
which modifications 41652 and 45749 have not been
embodied.
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A330-200
POST 43183
(54-3003)
This requirement is applicable to -200 PAX series aircraft on
which modification 43183 or SB 54-3003 has been embodied.
A330-200
POST 43183
(54-3003)
OR
A330-300
This requirement is applicable to -200 PAX series aircraft on
which modification 43183 or SB 54-3003 has been embodied
or all -300.
MSN 0001 – 0015
Requirement applicable to aircraft serial numbers 0001 to
0015 inclusive.
MSN 0114 – 9999
Requirement applicable to aircraft serial numbers 0114 and
subsequent.
RR
Requirement applicable to aircraft fitted with Rolls Royce
engines.
PRE 40610
Requirement applicable to aircraft on which modification
40610 has not been embodied.
POST 43500
PRE 46190
Requirement applicable to aircraft on which modification
43500 has been embodied and where modification 46190 has
not been embodied.
POST 44620
OR
POST 41833
Requirement applicable to aircraft on which modification
44620 has been embodied or where modification 41833 has
been embodied. The task is applicable if the aircraft is post
either mod.
POST 46190
S14212
This requirement is applicable to aircraft on which modification
46190 (with modification proposal S14212) has been
embodied.
Type 1
Door Type 1 = 1.60 m High, 0.61 m Wide - Emergency exit
type door.
Type A
Door Type A = 1.93 M High, 1.07 m Wide - Pax type door.
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10. MAINTENANCE TASK REPORTING SYSTEM
An Airbus database has been designed and dimensioned to receive data on a continuous flow basis.
Operators are therefore requested to report data from all maintenance checks. The data should include all
task results, findings and nil findings. The reporting and collection of nil-findings allows a computation of
finding rate (finding/nil-finding ratio) which may be used for future maintenance program optimization.
Refer to:
AirbusWorld > Content library > Maintenance and Engineering > Scheduled Maintenance Requirements >
MPD Reporting Templates.
This then gives access to the appropriate reporting spreadsheet.
Analysis of the reported data will enable Airbus to monitor the effectiveness of the Maintenance Program
and to further optimize it. Airlines who report data will also have the possibility to benchmark task findings
statistics against the reported data of other Airlines.
All reports should be sent to MPDtask.Reports@Airbus.com . Any related questions should be sent to the
same address. Operators will receive an acknowledgement for data reports.
Associated guideline can be found under:
Airbus World > App catalogue > IDOLS for Scheduled Maintenance > Support > MPD Task Reporting
Guidelines.
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11. GLOSSARY
APU Change (AC)
The interval term "APU Change" means the opportunity arising at some time between initiating removal of
an APU and completing installation of an APU, irrespective of whether the same APU is reinstalled or it is
replaced by a new or overhauled one.
APU Cycle(s) (CY)
A complete APU cycle.
APU Hour(s) (AH)
The APU operating time from start-up to shutdown.
Calendar Times (MO, YE)
Month(s) :
equivalent of 1 calendar month (can be calculated as 1/12 calendar year)
Year(s) :
equivalent of 12 calendar month (can be calculated as 365,25 days)
The time to "Start the clock" for the maintenance program for a particular aircraft is the delivery date to
the first operator, unless otherwise stated in any delivery documentation to the first operator.
Check
Task performed to ensure that a system or component is still serviceable (check of bottle weight, check of
firing circuit continuity, etc...) or that pressures or fluid levels are correct (See also visual check).
Visual Check (VCK)
An observation to determine that an item is fulfilling its intended purpose. Does not require quantitative
tolerances. This is a failure finding task.
Discard (DIS)
The removal from service of an item at a specified life limit.
Engine Change (EC)
The interval term "Engine Change" means the opportunity arising at some time between initiating removal
of an Engine and completing installation of an Engine, irrespective of whether the same Engine is
reinstalled or it is replaced by a new or overhauled one.
Engine Cycle(s) (CY)
A complete engine thermal cycle which includes the application of take-off power.
Flight Cycle(s) (FC)
A complete take-off and landing sequence.
Functional Check (FNC)
A quantitative check to determine if one or more functions of a system/sub system or component
performs, within specified limits.
This task may call for the use of special test equipment.
Inspection - Detailed: (DET)
An intensive examination of a specific item, installation or assembly to detect damage, failure or
irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity
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MAINTENANCE PLANNING DOCUMENT
deemed appropriate. Inspection aids such as mirrors, magnifying lenses etc. may be necessary. Surface
cleaning and elaborate access procedures may be required.
Inspection - General Visual: (GVI)
A visual examination of an interior or exterior area, installation or assembly to detect obvious damag e,
failure or irregularity. This level of inspection is made from within touching distance unless otherwise
specified. A mirror may be necessary to ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting conditions such as daylight, hangar lighting,
flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or
platforms may be required to gain proximity to the area being checked.
Inspection - Special Detailed: (SDI)
An intensive examination of a specific item, installation, or assembly to detect damage, failure or
irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or
equipment. Intricate cleaning and substantial access or disassembly procedure may be required. When
such inspections are required, detailed NDT procedures are described in the A330 Non destructive
Testing Manual (NTM).
Repeat Interval
The maximum permitted period (for all tasks not performed on a sampling basis) that can separate total
completion of a task from its next accomplishment.
Landing (LD)
An operation of an aircraft touching the runway and coming to a complete stop or performing a "touch an
go".
Lubrication (LUB)
Term covering all types of lubrication by grease gun, squirt can, spray, brush or hand application for the
purpose of maintaining the inherent design operating capabilities of an item.
Maintenance Task
An action or set of actions, including corresponding planning data, required to achieve a desired outcome
which maintains an item (component, system/sub system, structure) in or restores an item to serviceable
condition. This term includes inspection and determination of condition.
Maintenance Significant Item (MSI)
Item identified by the manufacturer, whose failure :
–
–
–
–
Could affect safety (ground or flight), and/or
Is undetectable or not likely to be detected during operation, and/or
Could have significant operational economic impact, and/or
Could have significant economic impact.
NDT-Inspection
Non-destructive inspection procedure, e.g. eddy current, ultra sonic.
Operational Check (OPC)
A task to determine qualitatively that an item is fulfilling its intended purpose. This task may include the
reading of the aircraft instruments but does not require the measurement of tolerances. This is a failure
finding task.
Replacement
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The action whereby an item is removed and another new or restored item is installed in its place.
Restoration (RST)
Term covering all actions (on/off the aircraft) necessary to return the item to a specific standard.
Sampling
The monitoring and/or withdrawal of selected devices from service to permit determination of their
condition at predetermined progressive intervals.
Structure Significant Item (SSI)
A structural detail, structural element or structural assembly which is judged significant by the
manufacturers because of the reduction in aircraft residual strength or loss of structural function which are
consequences of its failure.
Threshold
Limit deadline for all tasks not performed on a sampling basis at which the task must be accomplished for
the first time (subsequent accomplishment deadlines are obtained by adding the repeat interval and its
multiples to the threshold).
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ABBREVIATIONS
The following abbreviations are used through out the present document :
TERM
A/C
AC
AC
ACARS
ACMS
ACP
AD
ADF
ADIRU
ADR
AEVC
AFT
AH
AIB
AMM
AMTOSS
AOA
AOL
AOT
AOW
AP
APU
ARO
ASPSU
ATA
ATC
ATIMS
A/THR
ATT
BAT
BAC
BCL
BCRC
BITE
CESM
CFMI
CMP
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
CMR
CN
COMPT
CPCP
CRR
CSU
CVR
:
:
:
:
:
:
:
DEFINITION
Aircraft
Alternating Current
APU Change
Aircraft Communications Addressing & Reporting System
Aircraft Condition Monitoring System
Audio Control Panel
Airworthiness Directive
Automatic Direction Finder
Air Data / Inertial Reference Unit
Air Data Reference
Avionics Equipment Ventilation Computer
Rear or Average Flight Time
APU Operating Hours
Airbus
Aircraft Maintenance Manual
Aircraft Maintenance Task Oriented Support System
Angle of Attack
All Operators Letter
Alert Operators Transmission
All Operator Wire
Autopilot
Auxiliary Power Unit
Anti Roll Out
Autonomous Standby Power Supply Unit
ATA Specification
Air traffic control
Air Traffic and Information Management System
Autothrust
Attitude
Battery
Bulk Avionics Compartment
Battery Charge Limiter
Bulk Crew Rest Compartment
Built In Test Equipment
Commercial Engine Service Memorandum
CFM International
Configuration, Maintenance, Procedure and Dispatch Standards for Extended
Diversion Time Operations (ETOPS)
Certification Maintenance Requirements
Consigne de Navigabilité (French Airworthiness Directive)
Compartment
Corrosion Prevention and Control Program
Crew Rest Room
Command Sensor Unit
Cockpit Voice Recorder
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TERM
CY
D
DAR
DC
DFDR
DGAC
DET
DIS
DY
EC
ECAM
ECAS
EDP
EFCS
EFIS
EG
ELT
EMER
EMP
ENT.
ESM
ETOPS
EVAC
EWIS
EXTIR
FAA
F–BCRC
FC
FNC
FMP
FCOM
FCRC
FH
FOT
FWD
GCU
GLC
GPCU
GPWS
GSE
GRP x
GVI
HDG
HIRF
HR
IDG
IFE
IFEC
INTRO
IOR
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
DEFINITION
Cycle
Deleted
Digital ACMS Recorder
Direct Current
Digital Flight Data Recorder
Direction Générale de l’Aviation Civile (French Airworthiness Authority)
Detailed Inspection
Discard
Day
Engine Change
Electronic Centralized Aircraft Monitoring
Emergency Cabin Alert System
Engine Driven Pump
Electrical Flight Control System
Electronic Flight Instrument System
Entrance Guide
Emergency Locator Transmitter
Emergency
Engine Management Plan (RR engines)
Enterprise
Engine Shop Manual
Extended-range Twin-engine Operation Performance Standard
Evacuation
Electrical Wiring Interconnection System
Extinguisher
United States Federal Aviation Administration
Full Bulk Crew Rest Compartment
Flight Cycle
Functional Check
Fatigue Monitoring Program
Flight Crew Operating Manual
Flight Crew Rest Compt.
Flight Hours
Flight Operations Transmission
Forward
Generator Control Unit
Generator Line Contactor
Ground Power Control Unit
Ground Proximity Warning System
Ground Support Equipment
Weight variant group “x”
General Visual Inspection
Heading
High Intensity Radiated Fields
Hour
Integrated Drive Generator
Flight Entertainment
In Flight Entertainment Center
Introduction
Immediate Operational Request
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MAINTENANCE PLANNING DOCUMENT
TERM
ISB
ISIS
LD
LD
LDF
LDL
LDMCR
LED
LEP
LGCIU
LH
LUB
LTA
LWR
MAN
MCDU
MDCC
MH
MO
MOD
MORV
MPD
MPG
MRB
MSG
MSI
MSN
N
NDT
NR
NT
NTM
OIT
OPC
OTT
P-BCRC
PCU
PDU
POB
PREP
QAD
QAR
R
RA
RH
RMP
RR
RST
RSVR
S
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
DEFINITION
(Inspection) Service Bulletin
Integrated Stand By Instrument System
Landing
Lower Deck
Lower Deck Facility
Lower Deck Lavatory
Lower Deck Mobile Crew Rest
Light Emitting Diode
List of Effective Pages
Landing Gear Control and Interface Unit
Left Hand
Lubrication
German Airworthiness Directive
Lower
Manufacturer Advisory Notice (PW engines)
Multipurpose Control and Display Unit
Main Deck Cargo Compartment
Man hours
Month(s)
Modification
Mixer Overpressure Relief Valve
Maintenance Planning Document
Maintenance Planning Guide (PW engines)
Maintenance Review Board
Maintenance Steering Group
Maintenance Significant Item
Manufacturer Serial Number
New
Non Destructive Testing
National Requirements
Note
Non Destructive Testing Manual
Operators Information Transmission
Operational Check
Operator Training Transmission
Partial Bulk Crew Rest Compartment
Power Control Unit
Power Drive Unit
Pressure off Brakes
Preparation
Quick Attach Detach
Quick Access Recorder PA (Public Address)
Revised
Radio Altimeter
Right Hand
Radio Management Panel
Rolls Royce
Restoration
Reservoir
Sampling Size
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TERM
SEMR
SIL
SIU
SOV
SRM
SSA
SSI
STR
SYS
SVC
TBD
TCAS
THS
THSA
TOC
TPIS
TPS
TR
UD
ULB
VCK
VCC
VHF
VOR
VR
WGLQAR/DAR
WTB
WV
YE
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
:
DEFINITION
System Equipment Maintenance Requirements
Service Information Letter
Server Interface Unit
Shut off Valve
Structure Repair Manual
System Safety Assessment
Structure Significant Item
Stringer
System
Servicing
To be determined
Traffic Collision Avoidance System
Trimmable Horizontal Stabilizer
Trimmable Horizontal Stabiliser Actuator
Table of Content
Tire Pressure Indication System
Temporary Protection System
Temporary Revision
Upper deck
Underwater Locating Beacon
Visual Check
Video Control Center
Very High Frequency
VHF Omnibearing Range
Vendor Recommendation
Wireless Ground Link – Quick Access Recorder/Digital ACMS Recorder
: Wing Tip Brake
: Weight Variant
: Years
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ABBREVIATIONS
Page 4
MAINTENANCE PLANNING DOCUMENT
EFFECTIVITY CROSS REFERENCE TABLE
The following table shows the available status from September 2017:
Only the aircraft identified by an Airbus Manufacturer Serial Number (MSN) in the table are covered in this
document.
The following information is provided for each Aircraft:
•
•
•
•
•
•
•
Version Rank: Aircraft Rank within the customer versions (Example: XYZ02 0001, corresponds to first
aircraft within the second customer XYZ version).
Model: Aircraft Model
MSN: Manufacturer Serial Number
Registration: Aircraft Registration Number
STD: Aircraft Standard, corresponds to a production standard for a given aircraft technical definition
range.
Engine: Engine Model
Operator: Operator Name
Version
Rank
CPA01 0011
ITF01 0001
ITF01 0002
ITF01 0003
THA01 0002
I2L02 0001
I2L02 0002
THA01 0003
THA01 0004
I2L02 0003
LTU01 0001
I2L03 0001
Model
MSN
Registration
STD
Engine
Operator
330-342
330-301
330-301
330-301
330-321
330-301
330-301
330-321
330-321
330-301
330-322
330-322
0017
0030
0037
0045
0050
0054
0055
0060
0062
0070
0072
0082
B-HLK
OO-SFM
OO-SFN
OO-SFO
HS-TEA
9M-XAA
AP-BKL
HS-TEB
HS-TEC
AP-BKM
TC-OCA
OO-SFW
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
TRENT772-60
CF6-80E1A2
CF6-80E1A2
CF6-80E1A2
PW4164
CF6-80E1A2
CF6-80E1A2
PW4164
PW4164
CF6-80E1A2
PW4168
PW4168
CPA01 0002
ITF01 0005
LTU01 0002
LTU01 0003
I2L03 0002
330-342
330-301
330-322
330-322
330-322
0083
0086
0087
0095
0096
B-HLB
AP-BKN
TC-OCD
OO-SFV
OE-IAW
ST6
ST6
ST6
ST6
ST6
TRENT772-60
CF6-80E1A2
PW4168
PW4168
PW4168
CPA01 0004
HDA01 0002
CPA01 0005
HDA01 0003
THA01 0008
CPA01 0006
MAS01 0009
CPA01 0007
LTU01 0004
CPA01 0008
THA01 0009
LTU01 0005
HDA01 0004
GIA01 0001
GIA01 0002
I2L03 0003
330-342
330-342
330-342
330-342
330-321
330-342
330-322
330-342
330-322
330-342
330-321
330-322
330-342
330-341
330-341
330-322
0102
0106
0109
0111
0112
0113
0116
0118
0120
0121
0122
0127
0132
0138
0140
0143
B-HLD
B-HYB
B-HLE
C-GKTS
HS-TEG
B-HLF
EI-HEA
B-HLG
EI-FBU
B-HLH
HS-TEH
EI-HEB
C-GTSO
PK-GPA
PK-GPC
TC-OCC
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
ST6
TRENT772-60
TRENT772-60
TRENT772-60
TRENT772-60
PW4164
TRENT772-60
PW4168
TRENT772-60
PW4168
TRENT772-60
PW4164
PW4168
TRENT772-60
TRENT768-60
TRENT768-60
PW4168
CATHAY DRAGON
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
UNICAL AVIATION
GA TELESIS LLC
FINANCIAL INSTITUTIONS
UNICAL AVIATION
UNICAL AVIATION
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
CARLYLE AVIATION
PARTNERS
HAECO
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
CALC
CARLYLE AVIATION
PARTNERS
FINANCIAL INSTITUTIONS
CATHAY DRAGON
CATHAY DRAGON
AERCAP IRELAND LIMITED
KP AVIATION
CATHAY PACIFIC
ASL AIRLINES
CATHAY DRAGON
I FLY LTD
CATHAY PACIFIC
KP AVIATION
ASL AIRLINES
AERCAP IRELAND LIMITED
GARUDA INDONESIA
GARUDA INDONESIA
UNICAL AVIATION
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MAINTENANCE PLANNING DOCUMENT
Version
Rank
GIA01 0003
GIA01 0004
GIA01 0005
CPA01 0009
KAL01 0001
Model
MSN
Registration
STD
Engine
Operator
330-341
330-341
330-341
330-342
330-322
0144
0148
0153
0155
0162
PK-GPD
PK-GPE
PK-GPF
B-HLI
HL7550
ST6
ST6
ST6
ST6
ST6
TRENT768-60
TRENT768-60
TRENT768-60
TRENT772-60
PW4168
GIA01 0006
LTU01 0006
330-341
330-322
0165
0171
PK-GPG
EI-ETI
ST6
ST6
TRENT768-60
PW4168
KAL01 0002
330-322
0172
HL7551
ST6
PW4168
HDA01 0005
AUA04 0003
AUA04 0002
PAL03 0007
KAL01 0003
330-342
330-223
330-223
330-301
330-322
0177
0181
0195
0200
0206
C-GCTS
CS-TOH
CS-TOI
RP-C3337
HL7524
ST6
ST7
ST7
ST6
ST6
TRENT772-60
PW4168A
PW4168A
CF6-80E1A2
PW4168
THA01 0010
330-322
0209
HS-TEJ
ST6
PW4168
CMM01
0002
KAL01 0004
330-202
0211
CS-TQP
ST7
CF6-80E1A4
GARUDA INDONESIA
GARUDA INDONESIA
GARUDA INDONESIA
CATHAY DRAGON
KOREAN AIR LINES CO.
LTD
GARUDA INDONESIA
CARLYLE AVIATION
PARTNERS
KOREAN AIR LINES CO.
LTD
AERCAP IRELAND LIMITED
TAP AIR PORTUGAL
TAP AIR PORTUGAL
FINANCIAL INSTITUTIONS
KOREAN AIR LINES CO.
LTD
UNIVERSAL ASSET
MANAGEMENT
HI FLY
330-322
0219
HL7525
ST6
PW4168
KAL02 0001
330-223
0222
HL7538
ST7
PW4168A
AUA04 0001
THA01 0011
KAL02 0002
330-223
330-322
330-223
0223
0224
0226
CS-TOJ
HS-TEK
HL7539
ST7
ST6
ST7
PW4168A
PW4168
PW4168A
SWR01 0001
SAB02 0001
THA01 0012
HDA01 0006
SWR01 0002
KAL01 0005
330-223
330-223
330-322
330-342
330-223
330-322
0229
0230
0231
0234
0240
0241
OO-SFY
OY-GRN
EI-HEC
B-HYF
F-RARF
HL7540
ST7
ST7
ST6
ST6
ST7
ST6
PW4168A
PW4168A
PW4168
TRENT772-60
PW4168A
PW4168
CPA01 0012
330-342
0244
B-HLL
ST6
TRENT772-60
UAE01 0001
SWR01 0003
330-243
330-223
0248
0249
C-GJDA
OO-SFZ
ST7
ST7
TRENT772B-60
PW4168A
I2L10 0001
UAE01 0002
SWR01 0004
AIH01 0001
330-243
330-243
330-223
330-243
0250
0251
0253
0254
C-GGTS
C-GUFR
F-OFDF
G-MLJL
ST7
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
SWR01 0005
KAL03 0001
330-223
330-323
0255
0256
LZ-AWA
HL7554
ST7
ST8
PW4168A
PW4168A
KAL02 0003
330-223
0258
HL7552
ST7
PW4168A
MON01 0001
MON01 0002
AIH01 0002
330-243
330-243
330-243
0261
0265
0266
EC-MNY
EC-MJS
G-MDBD
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
KAL03 0002
330-323
0267
HL7553
ST8
PW4168A
ISSUE: JUL 01/21
Effectivity Cross Reference Table
KOREAN AIR LINES CO.
LTD
KOREAN AIR LINES CO.
LTD
TAP AIR PORTUGAL
UNICAL AVIATION
KOREAN AIR LINES CO.
LTD
FINANCIAL INSTITUTIONS
AIR GREENLAND
ASL AIRLINES
CATHAY DRAGON
DGA
KOREAN AIR LINES CO.
LTD
ARENA AVIATION
PARTNERS B.V.
AIR TRANSAT A.T. INC
ARENA AVIATION
PARTNERS B.V.
AIR TRANSAT A.T. INC
AIR TRANSAT A.T. INC
AIR CARAIBES
AJW CAPITAL PARTNERS
LTD
FINANCIAL INSTITUTIONS
KOREAN AIR LINES CO.
LTD
KOREAN AIR LINES CO.
LTD
ALTAVAIR LIMITED
ALTAVAIR LIMITED
AJW CAPITAL PARTNERS
LTD
KOREAN AIR LINES CO.
LTD
Page 2
MAINTENANCE PLANNING DOCUMENT
Version
Rank
EIN01 0001
I2L10 0002
CMM01
0003
SWR01 0007
GFA02 0001
ACA03 0001
ACA03 0002
GFA02 0002
UAE02 0001
ACA03 0003
CRL02 0001
GFA02 0003
GFA02 0004
SWR01 0008
Model
MSN
Registration
STD
Engine
Operator
330-202
330-243
330-202
0269
0271
0272
EI-LAX
C-GITS
EI-DIR
ST7
ST7
ST7
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
330-223
330-243
330-343
330-343
330-243
330-243
330-343
330-243
330-243
330-243
330-223
0275
0276
0277
0279
0281
0283
0284
0285
0286
0287
0288
VN-A371
A9C-KA
C-GFAF
C-GFAH
A9C-KB
EI-FNX
C-GFAJ
F-HCAT
A9C-KC
A9C-KD
D-ABXA
ST7
ST7
ST8
ST8
ST7
ST7
ST8
ST7
ST7
ST7
ST7
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4168A
SAB02 0002
SWR01 0009
330-223
330-223
0290
0291
LV-FNI
OO-SFT
ST7
ST7
PW4168A
PW4168A
UAE02 0002
UAE02 0003
SAB02 0003
SAB02 0004
AIH01 0003
330-243
330-243
330-223
330-223
330-243
0293
0295
0296
0300
0301
EI-FSE
EI-FSF
UR-WRQ
LV-FNJ
G-OMYT
ST7
ST7
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
PW4168A
PW4168A
TRENT772B-60
ALK02 0001
SWR01 0012
ALK02 0002
SWR01 0013
330-243
330-223
330-243
330-223
0303
0305
0306
0308
4R-ALA
CS-TOE
4R-ALB
CS-TOF
ST7
ST7
ST7
ST7
TRENT772B-60
PW4168A
TRENT772B-60
PW4168A
AIH01 0004
ALK02 0003
SWR01 0014
ALK02 0004
330-243
330-243
330-223
330-243
0309
0311
0312
0313
OY-VKF
4R-ALC
CS-TOG
4R-ALD
ST7
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
UAE02 0004
USA01 0001
UAE02 0005
330-243
330-323
330-243
0314
0315
0316
C-GUBF
N270AY
TC-OCL
ST7
ST8
ST7
TRENT772B-60
PW4168A
TRENT772B-60
AUA04 0004
CRL02 0002
SAB02 0005
USA01 0002
SAB02 0006
UAE02 0006
UAE02 0007
EIN01 0002
USA01 0003
GFA02 0005
USA01 0004
KAL03 0003
330-223
330-243
330-223
330-323
330-223
330-243
330-243
330-202
330-323
330-243
330-323
330-323
0317
0320
0322
0323
0324
0326
0328
0330
0333
0334
0337
0338
CS-TOK
F-HBIL
G-VLNM
N271AY
OO-SFU
SU-ALA
SU-ALB
EI-EWR
N272AY
A9C-KE
N273AY
HL7584
ST7
ST7
ST7
ST8
ST7
ST7
ST7
ST7
ST8
ST7
ST8
ST8
PW4168A
TRENT772B-60
PW4168A
PW4168A
PW4168A
TRENT772B-60
TRENT772B-60
CF6-80E1A4
PW4168A
TRENT772B-60
PW4168A
PW4168A
CMM01
0004
GFA02 0006
USA01 0005
330-202
0339
EI-DIP
ST7
CF6-80E1A4
AER LINGUS LTD
AIR TRANSAT A.T. INC
CARLYLE AVIATION
PARTNERS
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
AIR CANADA
AIR CANADA
AEROTRON LTD
I FLY LTD
AIR CANADA
CORSAIR S.A.
FINANCIAL INSTITUTIONS
FINANCIAL INSTITUTIONS
GE CAPITAL AVIATION
SERVICES
AEROLINEAS ARGENTINAS
GE CAPITAL AVIATION
SERVICES
I FLY LTD
I FLY LTD
FINANCIAL INSTITUTIONS
AEROLINEAS ARGENTINAS
AJW CAPITAL PARTNERS
LTD
SRILANKAN AIRLINES
CALC
SRILANKAN AIRLINES
ACS AERO MANAGEMENT
LIMITED
SUNCLASS AIRLINES A/S
SRILANKAN AIRLINES
AVTRADE LIMITED
CARLYLE AVIATION
PARTNERS
AIR TRANSAT A.T. INC
AMERICAN AIRLINES, INC.
TURKISH AIRLINES
TECHNIC
TAP AIR PORTUGAL
FINANCIAL INSTITUTIONS
VIRGIN ATLANTIC
AMERICAN AIRLINES, INC.
AIRCASTLE ADVISOR LLC
DAE CAPITAL
DAE CAPITAL
AERCAP IRELAND LIMITED
AMERICAN AIRLINES, INC.
FINANCIAL INSTITUTIONS
AMERICAN AIRLINES, INC.
KOREAN AIR LINES CO.
LTD
ALITALIA
330-243
330-323
0340
0342
A9C-KF
N274AY
ST7
ST8
TRENT772B-60
PW4168A
FINANCIAL INSTITUTIONS
AMERICAN AIRLINES, INC.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 3
MAINTENANCE PLANNING DOCUMENT
Version
Rank
SWR01 0015
ACA03 0004
UAE01 0003
Model
MSN
Registration
STD
Engine
Operator
330-223
330-343
330-243
0343
0344
0345
F-HHUB
C-GFUR
TC-OCG
ST7
ST8
ST7
PW4168A
TRENT772B-60
TRENT772B-60
THA02 0001
ALK02 0007
AIH02 0001
330-323
330-243
330-343
0346
0348
0349
HS-TEM
9H-NAW
OY-VKG
ST8
ST7
ST8
PW4168A
TRENT772B-60
TRENT772B-60
KAL03 0004
330-323
0350
HL7585
ST8
PW4168A
KAL03 0005
330-323
0351
HL7586
ST8
PW4168A
NVR01 0001
330-223
0353
TC-OCE
ST7
PW4168A
AIH02 0002
330-343
0356
OY-VKH
ST8
TRENT772B-60
AIH02 0003
RKA01 0001
NVR01 0002
RKA01 0002
ALK02 0008
SWR01 0016
330-343
330-223
330-223
330-223
330-243
330-223
0357
0358
0362
0364
0365
0366
OY-VKI
LV-FNK
TC-OCF
LV-FNL
PR-AIY
VN-A375
ST8
ST7
ST7
ST7
ST7
ST7
TRENT772B-60
PW4168A
PW4168A
PW4168A
TRENT772B-60
PW4168A
KAL03 0006
330-323
0368
HL7587
ST8
PW4168A
EDW01 0001
USA01 0006
ALK02 0009
USA01 0007
USA01 0008
UAE02 0008
UAE02 0009
CPA03 0001
USA01 0009
CPA03 0002
UAE02 0010
CPA03 0003
UAE02 0011
EIN01 0003
BMA01 0001
330-243
330-323
330-243
330-323
330-323
330-243
330-243
330-343
330-323
330-343
330-243
330-343
330-243
330-202
330-243
0369
0370
0372
0375
0380
0382
0384
0386
0388
0389
0392
0393
0396
0397
0398
N369BV
N275AY
PR-AIX
N276AY
N277AY
A6-EAD
A6-EAE
B-HLM
N278AY
B-HLN
SU-ALC
B-HLO
B-LHA
EI-DAA
G-CHTZ
ST7
ST8
ST7
ST8
ST8
ST7
ST7
ST8
ST8
ST8
ST7
ST8
ST7
ST7
ST7
TRENT772B-60
PW4168A
TRENT772B-60
PW4168A
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
ACA03 0005
BMA01 0002
LTU02 0001
330-343
330-243
330-223
0400
0401
0403
C-GHKR
G-WWBD
G-VMNK
ST8
ST7
ST7
TRENT772B-60
TRENT772B-60
PW4168A
BMA01 0003
330-243
0404
TC-OCK
ST7
TRENT772B-60
HDA02 0001
HDA02 0002
ACA03 0006
UAE02 0012
ACA03 0007
CPA04 0001
ACA03 0008
CPA04 0002
CPA04 0003
330-343
330-343
330-343
330-243
330-343
330-343
330-343
330-343
330-343
0405
0407
0408
0409
0412
0418
0419
0420
0421
B-HYG
C-GTSD
C-GHKW
JY-JVA
C-GHKX
B-HLP
C-GHLM
B-HLQ
B-HLR
ST8
ST8
ST8
ST7
ST8
ST8
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
AIR CARAIBES
AIR CANADA
ONUR HAVA TASIMACILIK
AWMS
KP AVIATION
AEROTRON LTD
SAN MARINO EXECUTIVE
AVIATION
KOREAN AIR LINES CO.
LTD
KOREAN AIR LINES CO.
LTD
ONUR HAVA TASIMACILIK
AWMS
SERES HAVACILIK SAN. VE
TIC. L
SUNCLASS AIRLINES A/S
AEROLINEAS ARGENTINAS
AIRCR.SALES & LEA.
AEROLINEAS ARGENTINAS
AZUL
CARLYLE AVIATION
PARTNERS
KOREAN AIR LINES CO.
LTD
AVOLON
AMERICAN AIRLINES, INC.
AZUL
AMERICAN AIRLINES, INC.
AMERICAN AIRLINES, INC.
EMIRATES
EMIRATES
CATHAY PACIFIC
AMERICAN AIRLINES, INC.
CATHAY PACIFIC
DAE CAPITAL
CATHAY PACIFIC
HONG KONG AIRLINES LTD
AER LINGUS LTD
AVIATION CAPITAL GROUP
LLC
AIR CANADA
FINANCIAL INSTITUTIONS
BBAM AIRCRAFT
MANAGEMENT LP
ONUR HAVA TASIMACILIK
AWMS
CATHAY PACIFIC
AIR TRANSAT A.T. INC
AIR CANADA
JORDAN AVIATION
AIR CANADA
CATHAY PACIFIC
AIR CANADA
CATHAY PACIFIC
CATHAY PACIFIC
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 4
MAINTENANCE PLANNING DOCUMENT
Version
Rank
AFR03 0001
CPA04 0004
KAL04 0001
Model
MSN
Registration
STD
Engine
Operator
330-203
330-343
330-323
0422
0423
0425
F-GZCA
B-HLS
HL7701
ST7
ST8
ST8
CF6-80E1A3
TRENT772B-60
PW4168A
JMC01 0001
KAL04 0002
330-243
330-323
0427
0428
C-GTSI
HL7702
ST7
ST8
TRENT772B-60
PW4168A
LTU03 0001
UAE02 0013
330-223
330-243
0432
0437
G-VMIK
TC-OCH
ST7
ST7
PW4168A
TRENT772B-60
CPA03 0004
QTR01 0005
AFR03 0002
LTU03 0002
AFR03 0003
UAE02 0014
UAE01 0004
LTU03 0003
BMA01 0004
JMC01 0002
AFR03 0004
C9G02 0001
UAE01 0005
G8E01 0002
330-343
330-202
330-203
330-223
330-203
330-243
330-243
330-223
330-243
330-243
330-203
330-243
330-243
330-203
0439
0441
0443
0444
0448
0451
0452
0454
0455
0456
0458
0461
0462
0463
B-HLT
EI-GEY
F-GZCB
F-HTIC
F-GZCC
P4-MLO
B-LHB
EC-MTT
C-GUBH
EI-GVH
F-GZCD
OE-IRD
PR-AIW
TC-JNF
ST8
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
TRENT772B-60
CF6-80E1A4
CF6-80E1A3
PW4168A
CF6-80E1A3
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772B-60
TRENT772B-60
CF6-80E1A3
AFR03 0005
G8E02 0001
LTU03 0004
G8E02 0002
330-203
330-202
330-223
330-202
0465
0466
0469
0472
F-GZCE
N478DM
EC-MTU
9H-BFS
ST7
ST7
ST7
ST7
CF6-80E1A3
CF6-80E1A4
PW4168A
CF6-80E1A4
QTR01 0001
330-202
0473
9H-RTU
ST7
CF6-80E1A4
LTU03 0005
G8E02 0003
330-223
330-203
0476
0477
G-VWND
CS-TOQ
ST7
ST7
PW4168A
CF6-80E1A3
HDA02 0003
TSC01 0001
AFR03 0006
KAL04 0003
330-343
330-243
330-203
330-323
0479
0480
0481
0484
B-HYI
C-GPTS
F-GZCF
HL7709
ST8
ST7
ST7
ST8
TRENT772B-60
TRENT772B-60
CF6-80E1A3
PW4168A
G8E02 0004
330-203
0486
CS-TOR
ST7
CF6-80E1A3
QTR02 0001
QTR01 0002
330-202
330-202
0487
0489
A7-HJJ
9H-PTN
ST7
ST7
CF6-80E1A4
CF6-80E1A4
KAL04 0004
330-323
0490
HL7710
ST8
PW4168A
UAE02 0015
330-243
0491
TC-OCM
ST7
TRENT772B-60
LTU03 0006
UAE02 0016
SAS02 0001
330-223
330-243
330-343
0493
0494
0496
F-HUNO
PR-AIU
LN-RKM
ST7
ST7
ST8
PW4168A
TRENT772B-60
TRENT772B-60
SAS02 0002
330-343
0497
LN-RKH
ST8
TRENT772B-60
AFR03 0007
330-203
0498
F-GZCG
ST7
CF6-80E1A3
AIR FRANCE
CATHAY PACIFIC
KOREAN AIR LINES CO.
LTD
AIR TRANSAT A.T. INC
KOREAN AIR LINES CO.
LTD
VIRGIN ATLANTIC
ONUR HAVA TASIMACILIK
AWMS
CATHAY PACIFIC
AER LINGUS LTD
AIR FRANCE
AERCAP IRELAND LIMITED
AIR FRANCE
GLOBAL JET ARUBA
HONG KONG AIRLINES LTD
WAMOS AIR
AIR TRANSAT A.T. INC
I FLY LTD
AIR FRANCE
AVOLON
AZUL
GE CAPITAL AVIATION
SERVICES
AIR FRANCE
AELF
WAMOS AIR
MALETH AERO AOC
LIMITED
BLUE PANORAMA
AIRLINES
VIRGIN ATLANTIC
GE CAPITAL AVIATION
SERVICES
CATHAY PACIFIC
AIR TRANSAT A.T. INC
AIR FRANCE
KOREAN AIR LINES CO.
LTD
GE CAPITAL AVIATION
SERVICES
QATAR AMIRI FLIGHT
BLUE PANORAMA
AIRLINES
KOREAN AIR LINES CO.
LTD
ONUR HAVA TASIMACILIK
AWMS
AIR CARAIBES
AZUL
SCANDINAVIAN AIRLINES
SYSTEM
SCANDINAVIAN AIRLINES
SYSTEM
AIR FRANCE
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 5
MAINTENANCE PLANNING DOCUMENT
Version
Rank
AFR03 0008
SEU01 0001
AFR03 0009
AFR03 0010
G8E01 0001
CYP01 0001
Model
MSN
Registration
STD
Engine
Operator
330-203
330-243
330-203
330-203
330-203
330-243
0500
0501
0502
0503
0504
0505
F-GZCH
TC-OCV
F-GZCI
F-GZCJ
D-AXGG
9S-ASJ
ST7
ST7
ST7
ST7
ST7
ST7
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
CF6-80E1A3
CF6-80E1A3
TRENT772B-60
QFA01 0003
ACI01 0001
QFA01 0001
UAE02 0017
330-202
330-202
330-202
330-243
0506
0507
0508
0509
VH-EBC
F-OHSD
VH-EBA
TC-OCN
ST7
ST7
ST7
ST7
CF6-80E1A4
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
ACI01 0002
QTR01 0003
HDA03 0001
QFA01 0004
SAS02 0003
330-202
330-202
330-343
330-202
330-343
0510
0511
0512
0513
0515
2-OJSE
EI-GGO
B-HYJ
VH-EBD
LN-RKO
ST7
ST7
ST8
ST7
ST8
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
AFR03 0011
UAE01 0006
AFR03 0012
QTR01 0004
330-203
330-243
330-203
330-202
0516
0518
0519
0521
F-GZCK
C-GUBC
F-GZCL
A7-ACR
ST7
ST7
ST7
ST7
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
QFA01 0002
NWA04 0001
UAE02 0018
330-202
330-323
330-243
0522
0524
0525
VH-EBB
N801NW
TC-OCO
ST7
ST8
ST7
CF6-80E1A4
PW4168A
TRENT772B-60
CYP01 0002
MEA01 0001
MEA01 0002
EVA01 0001
MEA01 0003
NWA04 0002
EVA01 0002
330-243
330-243
330-243
330-203
330-243
330-323
330-203
0526
0527
0529
0530
0532
0533
0535
EC-LQP
PR-AIZ
PR-AIT
D-AXGA
PR-AIV
N802NW
EI-GFZ
ST7
ST7
ST7
ST7
ST7
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772B-60
PW4168A
CF6-80E1A3
UAE02 0019
CPA03 0005
NWA04 0003
CPA03 0006
NWA04 0004
KAL04 0005
330-243
330-343
330-323
330-343
330-323
330-323
0536
0539
0542
0548
0549
0550
C-GUBD
B-HLU
N803NW
B-HLV
N804NW
HL7720
ST7
ST8
ST8
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
PW4168A
PW4168A
LDI01 0001
NWA04 0005
QFA03 0001
EVA02 0001
QFA03 0002
QFA03 0003
CPA04 0005
AFR03 0013
SAS02 0004
330-243
330-323
330-303
330-203
330-303
330-303
330-343
330-203
330-343
0551
0552
0553
0555
0558
0564
0565
0567
0568
EC-LNH
N805NW
VH-QPA
D-AXGC
VH-QPB
VH-QPC
B-HLW
F-GZCM
LN-RKN
ST7
ST8
ST8
ST7
ST8
ST8
ST8
ST7
ST8
TRENT772B-60
PW4168A
CF6-80E1A3
CF6-80E1A3
CF6-80E1A3
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
TRENT772B-60
DLH06 0001
QTR04 0001
EVA02 0002
QFA04 0004
330-343
330-202
330-203
330-303
0570
0571
0573
0574
OO-SFK
EI-GFX
D-AXGD
VH-QPD
ST8
ST7
ST7
ST8
TRENT772B-60
CF6-80E1A4
CF6-80E1A3
CF6-80E1A3
AIR FRANCE
AERCAP IRELAND LIMITED
AIR FRANCE
AIR FRANCE
LUFTHANSA TECHNIK AG
COMPAGNIE AFRICAINE
D'AVIAT.
QANTAS AIRWAYS LTD.
FINANCIAL INSTITUTIONS
QANTAS AIRWAYS LTD.
ONUR HAVA TASIMACILIK
AWMS
GA TELESIS LLC
FINANCIAL INSTITUTIONS
CATHAY PACIFIC
QANTAS AIRWAYS LTD.
SCANDINAVIAN AIRLINES
SYSTEM
AIR FRANCE
AIR TRANSAT A.T. INC
AIR FRANCE
QATAR AIRWAYS GROUP
Q.C.S.C.
QANTAS AIRWAYS LTD.
DELTA AIR LINES, INC.
ONUR HAVA TASIMACILIK
AWMS
AIRCASTLE ADVISOR LLC
AZUL
AZUL
LUFTHANSA TECHNIK AG
AZUL
DELTA AIR LINES, INC.
GENESIS AIRCRAFT
SERVICES LTD
AIR TRANSAT A.T. INC
CATHAY PACIFIC
DELTA AIR LINES, INC.
CATHAY PACIFIC
DELTA AIR LINES, INC.
KOREAN AIR LINES CO.
LTD
WAMOS AIR
DELTA AIR LINES, INC.
QANTAS AIRWAYS LTD.
LUFTHANSA TECHNIK AG
QANTAS AIRWAYS LTD.
QANTAS AIRWAYS LTD.
CATHAY PACIFIC
AIR FRANCE
SCANDINAVIAN AIRLINES
SYSTEM
BRUSSELS AIRLINES
FINANCIAL INSTITUTIONS
LUFTHANSA TECHNIK AG
QANTAS AIRWAYS LTD.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 6
MAINTENANCE PLANNING DOCUMENT
Version
Rank
DLH06 0002
Model
MSN
Registration
STD
Engine
Operator
330-343
0576
D-AIKB
ST8
TRENT772B-60
NWA04 0006
DLH06 0003
HDA04 0001
AFR03 0014
EVA02 0003
NWA04 0007
NWA04 0008
QFA04 0001
QFA04 0002
LDI01 0002
330-323
330-343
330-343
330-203
330-203
330-323
330-323
330-303
330-303
330-243
0578
0579
0581
0584
0587
0588
0591
0593
0595
0597
N806NW
OO-SFL
B-HYQ
F-GZCN
LV-GKO
N807NW
N808NW
VH-QPE
VH-QPF
F-HXXL
ST8
ST8
ST8
ST7
ST7
ST8
ST8
ST8
ST8
ST7
PW4168A
TRENT772B-60
TRENT772B-60
CF6-80E1A3
CF6-80E1A3
PW4168A
PW4168A
CF6-80E1A3
CF6-80E1A3
TRENT772B-60
MSR03 0001
CAL03 0001
QFA04 0003
QTR06 0001
CAL03 0002
NWA05 0001
MSR03 0002
QTR05 0001
NWA05 0002
QTR05 0002
NWA05 0003
NWA05 0004
NWA05 0005
QTR07 0001
330-243
330-302
330-303
330-202
330-302
330-223
330-243
330-203
330-223
330-203
330-223
330-223
330-223
330-302
0600
0602
0603
0605
0607
0609
0610
0612
0614
0616
0618
0620
0621
0623
SU-GCE
B-18301
VH-QPG
A7-HHM
B-18302
N851NW
SU-GCF
D-AXGE
N852NW
D-AXGF
N853NW
N854NW
N855NW
A7-AEA
ST7
ST8
ST8
ST7
ST8
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST8
TRENT772B-60
CF6-80E1A4
CF6-80E1A3
CF6-80E1A4
CF6-80E1A4
PW4168A
TRENT772B-60
CF6-80E1A3
PW4168A
CF6-80E1A3
PW4168A
PW4168A
PW4168A
CF6-80E1A4
IYE01 0001
330-243
0625
TC-OCI
ST7
TRENT772B-60
LDI01 0003
DLH06 0004
330-243
330-343
0627
0629
4R-ALH
D-AIKD
ST7
ST8
TRENT772B-60
TRENT772B-60
NWA05 0006
IYE01 0002
330-223
330-243
0631
0632
N856NW
TC-OCJ
ST7
ST7
PW4168A
TRENT772B-60
NWA05 0007
EVA02 0004
SEU01 0002
DLH06 0005
330-223
330-203
330-243
330-343
0633
0634
0635
0636
N857NW
LV-GKP
VP-BUC
D-AIKE
ST7
ST7
ST7
ST8
PW4168A
CF6-80E1A3
TRENT772B-60
TRENT772B-60
QTR07 0002
QTR08 0001
330-302
330-202
0637
0638
A7-AEB
A7-ACQ
ST8
ST7
CF6-80E1A4
CF6-80E1A4
AAR01 0001
CAL03 0003
DLH06 0006
330-323
330-302
330-343
0640
0641
0642
HL7736
B-18303
D-AIKF
ST8
ST8
ST8
PW4168A
CF6-80E1A4
TRENT772B-60
DAH01 0001
DLH06 0007
DAH01 0002
DLH06 0008
330-202
330-343
330-202
330-343
0644
0645
0647
0648
7T-VJV
OO-SFP
7T-VJW
D-AIKH
ST7
ST8
ST7
ST8
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CSN01 0001
330-243
0649
B-6056
ST7
TRENT772B-60
DAH01 0003
330-202
0650
7T-VJX
ST7
CF6-80E1A4
DEUTSCHE LUFTHANSA
AG
DELTA AIR LINES, INC.
BRUSSELS AIRLINES
CATHAY PACIFIC
AIR FRANCE
AEROLINEAS ARGENTINAS
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
QANTAS AIRWAYS LTD.
QANTAS AIRWAYS LTD.
AVIATOR CAPITAL
ACQUISITION CO
EGYPTAIR
CHINA AIRLINES LTD
QANTAS AIRWAYS LTD.
QATAR AMIRI FLIGHT
CHINA AIRLINES LTD
DELTA AIR LINES, INC.
EGYPTAIR
EW DISCOVER GMBH
DELTA AIR LINES, INC.
EW DISCOVER GMBH
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
QATAR AIRWAYS GROUP
Q.C.S.C.
ONUR HAVA TASIMACILIK
AWMS
SRILANKAN AIRLINES
DEUTSCHE LUFTHANSA
AG
DELTA AIR LINES, INC.
ONUR HAVA TASIMACILIK
AWMS
DELTA AIR LINES, INC.
AEROLINEAS ARGENTINAS
NORDWIND AIRLINES
DEUTSCHE LUFTHANSA
AG
AERCAP IRELAND LIMITED
QATAR AIRWAYS GROUP
Q.C.S.C.
ASIANA AIRLINES, INC.
CHINA AIRLINES LTD
DEUTSCHE LUFTHANSA
AG
AIR ALGERIE
BRUSSELS AIRLINES
AIR ALGERIE
DEUTSCHE LUFTHANSA
AG
CHINA SOUTHERN
AIRLINES
AIR ALGERIE
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 7
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CSN01 0002
Model
MSN
Registration
STD
Engine
Operator
330-243
0652
B-6057
ST7
TRENT772B-60
DAH01 0004
HDA05 0001
EVA02 0005
CSN01 0003
330-202
330-343
330-203
330-243
0653
0654
0655
0656
7T-VJY
9M-XXR
VQ-BMI
B-6058
ST7
ST8
ST7
ST7
CF6-80E1A4
TRENT772B-60
CF6-80E1A3
TRENT772B-60
AFR03 0015
ETD01 0001
QTR07 0003
330-203
330-243
330-302
0657
0658
0659
F-GZCO
A6-EYD
A7-AEC
ST7
ST7
ST8
CF6-80E1A3
TRENT772B-60
CF6-80E1A4
HDA05 0002
NWA04 0009
CSN01 0004
330-343
330-323
330-243
0662
0663
0664
HS-XTA
N809NW
B-6059
ST8
ST8
ST7
TRENT772B-60
PW4168A
TRENT772B-60
EEZ01 0001
330-223
0665
9M-MTU
ST7
PW4168A
MSR03 0003
DAH01 0005
CPA06 0001
IWD01 0001
CAL03 0004
CPA06 0002
NWA04 0010
CAL03 0005
AAR01 0002
EVA02 0007
330-243
330-202
330-342
330-343
330-302
330-342
330-323
330-302
330-323
330-203
0666
0667
0669
0670
0671
0673
0674
0675
0676
0678
SU-GCG
7T-VJZ
B-LAA
EC-LXA
B-18305
B-LAB
N810NW
B-18306
HL7740
B-16310
ST7
ST7
ST8
ST8
ST8
ST8
ST8
ST8
ST8
ST7
TRENT772B-60
CF6-80E1A4
TRENT772-60
TRENT772B-60
CF6-80E1A4
TRENT772-60
PW4168A
CF6-80E1A4
PW4168A
CF6-80E1A3
CPA07 0001
QTR10 0001
330-343
330-302
0679
0680
OO-SFH
A7-AED
ST8
ST8
TRENT772B-60
CF6-80E1A4
KLM01 0001
330-203
0682
PH-AOA
ST7
CF6-80E1A3
MSR03 0004
QTR05 0003
KLM01 0002
330-243
330-203
330-203
0683
0684
0686
SU-GCH
D-AXGB
PH-AOB
ST7
ST7
ST7
TRENT772B-60
CF6-80E1A3
CF6-80E1A3
DLH06 0009
330-343
0687
D-AIKI
ST8
TRENT772B-60
ETD01 0002
NWA04 0011
CAL03 0006
HDA06 0001
EVA02 0008
330-243
330-323
330-302
330-343
330-203
0688
0690
0691
0692
0693
A6-EYE
N811NW
B-18307
HS-XTC
B-16311
ST7
ST8
ST8
ST8
ST7
TRENT772B-60
PW4168A
CF6-80E1A4
TRENT772B-60
CF6-80E1A3
QFA04 0005
MSR03 0005
THY04 0001
CAL03 0007
TAM02 0001
330-303
330-243
330-203
330-302
330-202
0695
0696
0697
0699
0700
VH-QPH
SU-GCI
TC-JNA
B-18308
9H-MFS
ST8
ST7
ST7
ST8
ST7
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
CF6-80E1A4
DLH06 0010
KLM01 0003
330-343
330-203
0701
0703
OO-SFJ
PH-AOC
ST8
ST7
TRENT772B-60
CF6-80E1A3
THY04 0002
QFA04 0006
330-203
330-303
0704
0705
TC-JNB
VH-QPI
ST7
ST8
CF6-80E1A3
CF6-80E1A3
CHINA SOUTHERN
AIRLINES
AIR ALGERIE
AIRASIA X BERHAD
WNG CAPITAL LLC
CHINA SOUTHERN
AIRLINES
AIR FRANCE
ETIHAD AIRWAYS
QATAR AIRWAYS GROUP
Q.C.S.C.
AIRASIA X BERHAD
DELTA AIR LINES, INC.
CHINA SOUTHERN
AIRLINES
MALAYSIA AIRLINES
BERHAD
EGYPTAIR
AIR ALGERIE
CATHAY PACIFIC
EVELOP AIRLINES S.L.
CHINA AIRLINES LTD
CATHAY PACIFIC
DELTA AIR LINES, INC.
CHINA AIRLINES LTD
ASIANA AIRLINES, INC.
EVA AIRWAYS
CORPORATION
BRUSSELS AIRLINES
QATAR AIRWAYS GROUP
Q.C.S.C.
KLM ROYAL DUTCH
AIRLINES
EGYPTAIR
EW DISCOVER GMBH
KLM ROYAL DUTCH
AIRLINES
DEUTSCHE LUFTHANSA
AG
ETIHAD AIRWAYS
DELTA AIR LINES, INC.
CHINA AIRLINES LTD
AIRASIA X BERHAD
EVA AIRWAYS
CORPORATION
QANTAS AIRWAYS LTD.
AJWAA AIRLINES
TURKISH AIRLINES CO.
CHINA AIRLINES LTD
MALETH AERO AOC
LIMITED
BRUSSELS AIRLINES
KLM ROYAL DUTCH
AIRLINES
TURKISH AIRLINES CO.
QANTAS AIRWAYS LTD.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 8
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CAL03 0008
AAR01 0003
MSR03 0006
QTR10 0002
Model
MSN
Registration
STD
Engine
Operator
330-302
330-323
330-243
330-302
0707
0708
0709
0711
B-18309
HL7741
SU-GCJ
A7-AEE
ST8
ST8
ST7
ST8
CF6-80E1A4
PW4168A
TRENT772B-60
CF6-80E1A4
QFA04 0007
CES03 0001
CAL03 0009
HDA06 0002
ETD04 0001
NWA05 0008
CES03 0002
QTR10 0003
330-303
330-343
330-302
330-343
330-243
330-223
330-343
330-302
0712
0713
0714
0716
0717
0718
0720
0721
VH-QPJ
G-EODS
B-18310
9M-XXQ
A6-EYF
N858NW
HS-XTG
A7-AEF
ST8
ST8
ST8
ST8
ST7
ST7
ST8
ST8
CF6-80E1A3
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
CF6-80E1A4
NWA05 0009
ETD04 0002
CAL03 0010
MSR03 0007
CES04 0001
ETD04 0004
ETD04 0003
CES04 0002
AEA01 0001
QTR10 0004
330-223
330-243
330-302
330-243
330-243
330-243
330-243
330-243
330-202
330-302
0722
0724
0725
0726
0728
0729
0730
0732
0733
0734
N859NW
A6-EYG
B-18351
SU-GCK
C-GUBL
A6-EYH
A6-EYI
C-GUBT
AP-BNE
A7-AEG
ST7
ST7
ST8
ST7
ST7
ST7
ST7
ST7
ST7
ST8
PW4168A
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
CES04 0003
ETD04 0005
KLM01 0004
330-243
330-243
330-203
0735
0737
0738
B-6123
A6-EYJ
PH-AOD
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
CF6-80E1A3
LTU04 0001
HDA06 0003
THY04 0003
QTR11 0001
330-223
330-343
330-203
330-202
0739
0741
0742
0743
EI-GCZ
EC-NOF
TC-JNC
A7-ACG
ST7
ST8
ST7
ST7
PW4168A
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
AEA01 0002
330-202
0745
TF-EAD
ST7
CF6-80E1A4
QTR11 0002
330-202
0746
A7-ACI
ST7
CF6-80E1A4
ASY01 0001
330-203
0747
A39-001
ST7
CF6-80E1A3
AEA01 0003
330-202
0749
TF-EAC
ST7
CF6-80E1A4
CCA02 0001
JAI01 0001
CAL03 0011
THY04 0004
EVA02 0009
330-243
330-243
330-302
330-203
330-203
0750
0751
0752
0754
0755
B-6070
DQ-FJO
B-18311
TC-JND
B-16312
ST7
ST7
ST8
ST7
ST7
TRENT772C-60
TRENT772B-60
CF6-80E1A4
CF6-80E1A3
CF6-80E1A3
CCA02 0002
FWI02 0001
CCA02 0003
QTR11 0003
330-243
330-323
330-243
330-202
0756
0758
0759
0760
B-6071
F-ORLY
B-6072
A7-ACJ
ST7
ST8
ST7
ST7
TRENT772C-60
PW4168A
TRENT772C-60
CF6-80E1A4
CAL03 0012
KLM01 0005
330-302
330-203
0769
0770
LY-LEO
PH-AOE
ST8
ST7
CF6-80E1A4
CF6-80E1A3
CHINA AIRLINES LTD
ASIANA AIRLINES, INC.
EGYPTAIR
QATAR AIRWAYS GROUP
Q.C.S.C.
QANTAS AIRWAYS LTD.
TITAN AIRWAYS LTD
CHINA AIRLINES LTD
AIRASIA X BERHAD
ETIHAD AIRWAYS
DELTA AIR LINES, INC.
AIRASIA X BERHAD
QATAR AIRWAYS GROUP
Q.C.S.C.
DELTA AIR LINES, INC.
ETIHAD AIRWAYS
CHINA AIRLINES LTD
EGYPTAIR
AIR TRANSAT A.T. INC
ETIHAD AIRWAYS
ETIHAD AIRWAYS
AIR TRANSAT A.T. INC
SERENE AIR
QATAR AIRWAYS GROUP
Q.C.S.C.
AEROTRON LTD
ETIHAD AIRWAYS
KLM ROYAL DUTCH
AIRLINES
I FLY LTD
WAMOS AIR
TURKISH AIRLINES CO.
QATAR AIRWAYS GROUP
Q.C.S.C.
GE CAPITAL AVIATION
SERVICES
QATAR AIRWAYS GROUP
Q.C.S.C.
ROYAL AUSTRALIAN AIR
FORCE
GE CAPITAL AVIATION
SERVICES
AIR CHINA LIMITED
AIR PACIFIC LIMITED
CHINA AIRLINES LTD
TURKISH AIRLINES CO.
EVA AIRWAYS
CORPORATION
AIR CHINA LIMITED
AIR CARAIBES
AIR CHINA LIMITED
QATAR AIRWAYS GROUP
Q.C.S.C.
GETJET AIRLINES UAB
KLM ROYAL DUTCH
AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 9
MAINTENANCE PLANNING DOCUMENT
Version
Rank
AAR01 0004
CES03 0003
THY04 0005
CPA07 0002
CES03 0004
NWA05 0010
CCA03 0001
CES03 0005
CES03 0006
NWA04 0012
CCA03 0002
HDA05 0003
ETD02 0001
QTR10 0005
CES03 0007
QTR11 0004
Model
MSN
Registration
STD
Engine
Operator
330-323
330-343
330-203
330-342
330-343
330-223
330-243
330-343
330-343
330-323
330-243
330-343
330-243
330-302
330-343
330-202
0772
0773
0774
0776
0777
0778
0780
0781
0782
0784
0785
0786
0788
0789
0791
0792
HL7746
HS-XTH
TC-JNE
B-LAD
B-LDR
N860NW
B-6073
B-LDQ
9M-XBE
N812NW
B-6075
EC-NOG
A6-EYK
EI-EIK
HS-XTJ
A7-ACK
ST8
ST8
ST7
ST8
ST8
ST7
ST7
ST8
ST8
ST8
ST7
ST8
ST7
ST8
ST8
ST7
PW4168A
TRENT772B-60
CF6-80E1A3
TRENT772-60
TRENT772B-60
PW4168A
TRENT772C-60
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TCX01 0001
NWA05 0011
CCA03 0003
NWA04 0013
KLM01 0006
330-243
330-223
330-243
330-323
330-203
0795
0796
0797
0799
0801
C-GTSJ
N861NW
B-6076
N813NW
PH-AOF
ST7
ST7
ST7
ST8
ST7
TRENT772B-60
PW4168A
TRENT772C-60
PW4168A
CF6-80E1A3
EEZ02 0001
AAR01 0005
CAL03 0013
NWA04 0014
JAI01 0002
ETD02 0002
CCA03 0004
KLM01 0007
QTR10 0006
330-223
330-323
330-302
330-323
330-243
330-243
330-243
330-203
330-302
0802
0803
0805
0806
0807
0809
0810
0811
0813
OE-ISK
HL7747
B-18352
N814NW
DQ-FJP
A6-EYL
B-6079
LZ-ONE
A7-AEI
ST7
ST8
ST8
ST8
ST7
ST7
ST7
ST7
ST8
PW4168A
PW4168A
CF6-80E1A4
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772C-60
CF6-80E1A3
CF6-80E1A4
AEA01 0004
CCA03 0005
NWA04 0015
CSN01 0005
KLM01 0008
QTR11 0005
330-202
330-243
330-323
330-243
330-203
330-202
0814
0815
0817
0818
0819
0820
EC-JZL
B-6080
N815NW
EC-NBN
AP-BNF
A7-ACL
ST7
ST7
ST8
ST7
ST7
ST7
CF6-80E1A4
TRENT772C-60
PW4168A
TRENT772C-60
CF6-80E1A3
CF6-80E1A4
CES04 0004
EEZ01 0002
330-243
330-223
0821
0822
B-6082
9M-MTV
ST7
ST7
TRENT772B-60
PW4168A
CAL03 0014
ETD02 0003
JAI02 0001
QTR10 0007
330-302
330-243
330-202
330-302
0823
0824
0825
0826
B-18315
A6-EYM
I-EJGA
A7-AEJ
ST8
ST7
ST7
ST8
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
NWA04 0016
LTU04 0002
330-323
330-223
0827
0828
N816NW
9M-MTW
ST8
ST7
PW4168A
PW4168A
CES03 0008
JAI02 0002
ETD02 0004
IWD01 0002
KLM01 0009
330-343
330-202
330-243
330-343
330-203
0830
0831
0832
0833
0834
B-6083
I-EJGB
A6-EYN
CS-TRH
JY-JVB
ST8
ST7
ST7
ST8
ST7
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CF6-80E1A3
ASIANA AIRLINES, INC.
AIRASIA X BERHAD
TURKISH AIRLINES CO.
CATHAY PACIFIC
AIR HONG KONG LTD
DELTA AIR LINES, INC.
AIR CHINA LIMITED
AIR HONG KONG LTD
AIRASIA X BERHAD
DELTA AIR LINES, INC.
AIR CHINA LIMITED
WAMOS AIR
ETIHAD AIRWAYS
AER LINGUS LTD
AIRASIA X BERHAD
QATAR AIRWAYS GROUP
Q.C.S.C.
AIR TRANSAT A.T. INC
DELTA AIR LINES, INC.
AIR CHINA LIMITED
DELTA AIR LINES, INC.
KLM ROYAL DUTCH
AIRLINES
AVOLON
ASIANA AIRLINES, INC.
CHINA AIRLINES LTD
DELTA AIR LINES, INC.
AIR PACIFIC LIMITED
ETIHAD AIRWAYS
AIR CHINA LIMITED
GULLIVAIR LTD
QATAR AIRWAYS GROUP
Q.C.S.C.
DEUCALION AVIATION LTD
AIR CHINA LIMITED
DELTA AIR LINES, INC.
WAMOS AIR
SERENE AIR
QATAR AIRWAYS GROUP
Q.C.S.C.
CHINA EASTERN AIRLINES
MALAYSIA AIRLINES
BERHAD
CHINA AIRLINES LTD
ETIHAD AIRWAYS
ETIHAD AIRWAYS
QATAR AIRWAYS GROUP
Q.C.S.C.
DELTA AIR LINES, INC.
MALAYSIA AIRLINES
BERHAD
CHINA EASTERN AIRLINES
ETIHAD AIRWAYS
ETIHAD AIRWAYS
ORBEST S.A.
JORDAN AVIATION
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 10
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CES03 0009
CAL03 0015
CCA02 0004
CSN01 0006
EIN02 0001
QFA05 0001
NWA04 0017
AAR01 0006
EIN03 0001
QTR11 0006
Model
MSN
Registration
STD
Engine
Operator
330-343
330-302
330-243
330-243
330-202
330-202
330-323
330-323
330-302
330-202
0836
0838
0839
0840
0841
0842
0843
0845
0847
0849
B-6085
B-18316
B-6081
EC-NCK
EI-DUO
VH-EBE
N817NW
HL7754
EI-DUZ
A7-ACM
ST8
ST8
ST7
ST7
ST7
ST7
ST8
ST8
ST8
ST7
TRENT772B-60
CF6-80E1A4
TRENT772C-60
TRENT772C-60
CF6-80E1A4
CF6-80E1A4
PW4168A
PW4168A
CF6-80E1A4
CF6-80E1A4
CPA08 0001
CES03 0010
ETD02 0005
QFA05 0002
ETD02 0006
CPA08 0002
NWA04 0018
NWA04 0019
NWA04 0020
CCA03 0006
CAL03 0016
CES03 0011
97X01 0001
330-342
330-343
330-243
330-202
330-243
330-342
330-323
330-323
330-323
330-243
330-302
330-343
330-243
0850
0851
0852
0853
0854
0855
0857
0858
0859
0860
0861
0862
0863
B-LAE
B-6095
A6-EYO
VH-EBF
A6-EYP
B-LAF
N818NW
N819NW
N820NW
B-6090
B-18317
B-6096
UP-A3001
ST8
ST8
ST7
ST7
ST7
ST8
ST8
ST8
ST8
ST7
ST8
ST8
ST7
TRENT772-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772-60
PW4168A
PW4168A
PW4168A
TRENT772C-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
NWA04 0021
CES03 0012
CCA03 0007
ETD04 0006
TAM03 0001
46W01 0001
330-323
330-343
330-243
330-243
330-223
330-203
0865
0866
0867
0868
0869
0871
N821NW
B-6097
B-6091
A6-EYQ
TC-JIO
9H-LFS
ST8
ST8
ST7
ST7
ST7
ST7
PW4168A
TRENT772B-60
TRENT772C-60
TRENT772B-60
PW4168A
CF6-80E1A3
CCA03 0008
KFR01 0001
68W01 0001
TAM03 0002
TAP02 0001
CSN02 0001
68W01 0002
JAI02 0003
MAU03 0001
CCA03 0009
JAI02 0004
QFA06 0001
JAI02 0005
CSN02 0002
CCA03 0010
KFR01 0002
330-243
330-223
330-243
330-223
330-202
330-343
330-243
330-203
330-202
330-243
330-202
330-203
330-202
330-343
330-243
330-223
0873
0874
0875
0876
0877
0879
0881
0882
0883
0884
0885
0887
0888
0889
0890
0891
B-6092
LZ-AWZ
B-6116
TC-JIP
CS-TOL
TC-MCM
B-6118
TC-JIL
3B-NBM
B-6093
YU-ARA
VH-EBG
VT-JWW
TC-MCN
B-6113
5N-JIC
ST7
ST7
ST7
ST7
ST7
ST8
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST8
ST7
ST7
TRENT772C-60
PW4168A
TRENT772B-60
PW4168A
CF6-80E1A4
TRENT772C-60
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
TRENT772C-60
CF6-80E1A4
CF6-80E1A3
CF6-80E1A4
TRENT772C-60
TRENT772C-60
PW4168A
QFA06 0002
330-203
0892
A39-006
ST7
CF6-80E1A3
QTR10 0008
CPA08 0003
DLH08 0001
330-302
330-343
330-343
0893
0895
0896
EI-EIL
OO-SFC
D-AIKK
ST8
ST8
ST8
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CHINA EASTERN AIRLINES
CHINA AIRLINES LTD
AIR CHINA LIMITED
WAMOS AIR
AER LINGUS LTD
QANTAS AIRWAYS LTD.
DELTA AIR LINES, INC.
ASIANA AIRLINES, INC.
AER LINGUS LTD
QATAR AIRWAYS GROUP
Q.C.S.C.
CATHAY PACIFIC
CHINA EASTERN AIRLINES
ETIHAD AIRWAYS
QANTAS AIRWAYS LTD.
ETIHAD AIRWAYS
CATHAY PACIFIC
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
AIR CHINA LIMITED
CHINA AIRLINES LTD
CHINA EASTERN AIRLINES
STATE AIR COMPANY
BERKUT
DELTA AIR LINES, INC.
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
ETIHAD AIRWAYS
TURKISH AIRLINES CO.
MALETH AERO AOC
LIMITED
AIR CHINA LIMITED
GULLIVAIR LTD
HAINAN AIRLINES
TURKISH AIRLINES CO.
TAP AIR PORTUGAL
MNG AIRLINES
HAINAN AIRLINES
TRUEAERO LLC
AIR MAURITIUS
AIR CHINA LIMITED
AIR SERBIA
QANTAS AIRWAYS LTD.
JET AIRWAYS
MNG AIRLINES
AIR CHINA LIMITED
PEMBROKE CAPITAL
LIMITED
ROYAL AUSTRALIAN AIR
FORCE
AER LINGUS LTD
BRUSSELS AIRLINES
DEUTSCHE LUFTHANSA
AG
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 11
MAINTENANCE PLANNING DOCUMENT
Version
Rank
QFA06 0003
Model
MSN
Registration
STD
Engine
Operator
330-203
0898
A39-007
ST7
CF6-80E1A3
TAP02 0002
KLM01 0010
JAI02 0006
CCA03 0011
TAP02 0003
DLH08 0002
330-202
330-203
330-203
330-243
330-202
330-343
0899
0900
0901
0903
0904
0905
CS-TOM
AP-BNG
TC-JIM
B-6117
CS-TON
D-AIKL
ST7
ST7
ST7
ST7
ST7
ST8
CF6-80E1A4
CF6-80E1A3
CF6-80E1A3
TRENT772C-60
CF6-80E1A4
TRENT772B-60
68W01 0003
QTR10 0009
330-243
330-302
0906
0907
B-6088
A7-AEN
ST7
ST8
TRENT772B-60
CF6-80E1A4
CSN02 0003
330-343
0908
9H-SMA
ST8
TRENT772C-60
CCA03 0012
LTU05 0001
330-243
330-223
0909
0911
B-6115
9M-MTX
ST7
ST7
TRENT772C-60
PW4168A
DLH08 0003
330-343
0913
D-AIKM
ST8
TRENT772B-60
TAP02 0004
CPA08 0004
CES04 0005
QTR10 0010
330-202
330-343
330-243
330-302
0914
0915
0916
0918
CS-TOO
OO-SFB
B-6099
A7-AEO
ST7
ST8
ST7
ST8
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CF6-80E1A4
68W01 0004
CAL03 0017
DLH08 0004
330-243
330-302
330-343
0919
0920
0922
B-6089
B-18353
D-AIKN
ST7
ST8
ST8
TRENT772B-60
CF6-80E1A4
TRENT772B-60
JAI02 0007
KLM04 0001
330-202
330-203
0923
0925
VT-JWV
PH-AON
ST7
ST7
CF6-80E1A4
CF6-80E1A3
MEA02 0001
KFR01 0003
330-243
330-223
0926
0927
OD-MED
5N-JID
ST7
ST7
TRENT772B-60
PW4168A
CES03 0013
CCA03 0013
AEA01 0005
JAI02 0008
TAP02 0005
CSN02 0004
CES03 0014
CSN02 0005
330-343
330-243
330-202
330-203
330-202
330-343
330-343
330-343
0928
0930
0931
0932
0934
0935
0936
0937
B-6100
B-6130
EC-KOM
TC-JIN
CS-TOP
EC-NHM
B-6506
9H-SMC
ST8
ST7
ST7
ST7
ST7
ST8
ST8
ST8
TRENT772B-60
TRENT772C-60
CF6-80E1A4
CF6-80E1A3
CF6-80E1A4
TRENT772C-60
TRENT772B-60
TRENT772B-60
KFR01 0004
QFA05 0003
CCA03 0014
CES03 0015
51W01 0001
330-223
330-202
330-243
330-343
330-223
0939
0940
0941
0942
0943
LZ-AWY
VH-EBJ
B-6131
B-6507
VN-A376
ST7
ST7
ST7
ST8
ST7
PW4168A
CF6-80E1A4
TRENT772C-60
TRENT772B-60
PW4168A
CCA03 0015
QFA05 0004
KFR01 0005
JAI02 0009
AVA01 0001
330-243
330-202
330-223
330-202
330-243
0944
0945
0946
0947
0948
B-6132
VH-EBK
EI-GCU
2-ACUA
G-TCXB
ST7
ST7
ST7
ST7
ST7
TRENT772C-60
CF6-80E1A4
PW4168A
CF6-80E1A4
TRENT772B-60
TAM03 0003
330-223
0949
TC-JIR
ST7
PW4168A
ROYAL AUSTRALIAN AIR
FORCE
TAP AIR PORTUGAL
SERENE AIR
TURKISH AIRLINES CO.
AIR CHINA LIMITED
TAP AIR PORTUGAL
DEUTSCHE LUFTHANSA
AG
HAINAN AIRLINES
QATAR AIRWAYS GROUP
Q.C.S.C.
SMARTLYNX AIRLINES
MALTA
AIR CHINA LIMITED
MALAYSIA AIRLINES
BERHAD
DEUTSCHE LUFTHANSA
AG
TAP AIR PORTUGAL
BRUSSELS AIRLINES
CHINA EASTERN AIRLINES
QATAR AIRWAYS GROUP
Q.C.S.C.
HAINAN AIRLINES
CHINA AIRLINES LTD
DEUTSCHE LUFTHANSA
AG
JET AIRWAYS
KLM ROYAL DUTCH
AIRLINES
MIDDLE EAST AIRLINES
PEMBROKE CAPITAL
LIMITED
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
AIR EUROPA
TURKISH AIRLINES CO.
TAP AIR PORTUGAL
WAMOS AIR
CHINA EASTERN AIRLINES
SMARTLYNX AIRLINES
MALTA
GULLIVAIR LTD
QANTAS AIRWAYS LTD.
AIR CHINA LIMITED
CHINA EASTERN AIRLINES
MACQUARIE AIRCRAFT
LEASING LTD
AIR CHINA LIMITED
QANTAS AIRWAYS LTD.
I FLY LTD
ALTAVAIR LIMITED
AVIATION CAPITAL GROUP
LLC
TURKISH AIRLINES CO.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 12
MAINTENANCE PLANNING DOCUMENT
Version
Rank
AEA01 0006
ASY01 0002
Model
MSN
Registration
STD
Engine
Operator
330-202
330-203
0950
0951
EC-KTG
A39-002
ST7
ST7
CF6-80E1A4
CF6-80E1A3
XFA01 0001
CSN02 0006
330-343
330-343
0952
0954
9M-XXA
9H-SME
ST8
ST8
TRENT772B-60
TRENT772B-60
JAI02 0010
CCA03 0016
CSN02 0007
330-202
330-243
330-343
0956
0957
0958
2-ACUB
B-6505
B-6502
ST7
ST7
ST8
CF6-80E1A4
TRENT772C-60
TRENT772B-60
CPA08 0005
TAM03 0004
51W01 0002
330-343
330-223
330-223
0959
0961
0962
OO-SFD
TC-JIS
VN-A377
ST8
ST7
ST7
TRENT772B-60
PW4168A
PW4168A
AFL01 0001
CSN02 0008
330-243
330-343
0963
0964
VP-BLX
B-6501
ST7
ST8
TRENT772B-60
TRENT772B-60
FWI02 0002
XLA01 0001
AVA01 0002
330-323
330-243
330-243
0965
0966
0967
EI-GPJ
C-GTSR
G-TCXC
ST8
ST7
ST7
PW4168A
TRENT772B-60
TRENT772B-60
TAM03 0005
330-223
0968
9M-MTY
ST7
PW4168A
ASY01 0003
330-203
0969
A39-003
ST7
CF6-80E1A3
51W01 0003
XLA01 0002
AFL01 0002
XFA01 0002
ETD07 0001
QFA06 0004
TAM03 0006
SIA04 0001
51W01 0004
RSF01 0001
68W01 0005
SIA04 0002
MEA02 0002
EIN03 0002
SIA04 0003
68W01 0006
DLH08 0005
330-223
330-243
330-243
330-343
330-243
330-203
330-223
330-343
330-223
330-202
330-243
330-343
330-243
330-302
330-343
330-243
330-343
0970
0971
0973
0974
0975
0976
0977
0978
0979
0980
0982
0983
0984
0985
0986
0988
0989
CS-TRY
C-GTSZ
YU-ARB
9M-XXB
A6-EYR
VH-EBL
TC-JIT
HS-XTI
VP-BUA
2401
B-6133
OO-SFG
OD-MEA
EI-EAV
C-GHKC
B-8549
D-AIKO
ST7
ST7
ST7
ST8
ST7
ST7
ST7
ST8
ST7
ST7
ST7
ST8
ST7
ST8
ST8
ST7
ST8
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
PW4168A
TRENT772B-60
PW4168A
CF6-80E1A4
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
THA07 0001
330-343
0990
HS-TEN
ST8
TRENT772B-60
ETD07 0002
XLA01 0003
FIN02 0001
MEA02 0004
RSF01 0002
SIA04 0004
MEA02 0003
SWR03 0001
AAR02 0001
51W01 0005
330-243
330-243
330-302
330-243
330-202
330-343
330-243
330-343
330-323
330-223
0991
0992
0994
0995
0996
0997
0998
1000
1001
1002
A6-EYS
EC-MAJ
OH-LTM
OD-MEC
2402
C-GEFA
OD-MEB
HB-JHA
HL7792
VP-BUB
ST7
ST7
ST8
ST7
ST7
ST8
ST7
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4168A
PW4168A
AIR EUROPA
ROYAL AUSTRALIAN AIR
FORCE
AIRASIA X BERHAD
SMARTLYNX AIRLINES
MALTA
ALTAVAIR LIMITED
AIR CHINA LIMITED
CHINA SOUTHERN
AIRLINES
BRUSSELS AIRLINES
TURKISH AIRLINES CO.
MACQUARIE AIRCRAFT
LEASING LTD
AERCAP IRELAND LIMITED
CHINA SOUTHERN
AIRLINES
I FLY LTD
AIR TRANSAT A.T. INC
AVIATION CAPITAL GROUP
LLC
MALAYSIA AIRLINES
BERHAD
ROYAL AUSTRALIAN AIR
FORCE
AELF
AIR TRANSAT A.T. INC
AIR SERBIA
AIRASIA X BERHAD
AVOLON
QANTAS AIRWAYS LTD.
TURKISH AIRLINES CO.
AIRASIA X BERHAD
NORDWIND AIRLINES
ROYAL SAUDI AIR FORCE
HAINAN AIRLINES
BRUSSELS AIRLINES
MIDDLE EAST AIRLINES
AER LINGUS LTD
AIR CANADA
BEIJING CAPITAL AIRLINES
DEUTSCHE LUFTHANSA
AG
THAI AIRWAYS
INTERNATIONAL
AVOLON
WAMOS AIR
FINNAIR OYJ
MIDDLE EAST AIRLINES
ROYAL SAUDI AIR FORCE
AIR CANADA
MIDDLE EAST AIRLINES
SWISS
ASIANA AIRLINES, INC.
NORDWIND AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 13
MAINTENANCE PLANNING DOCUMENT
Version
Rank
THA07 0002
Model
MSN
Registration
STD
Engine
Operator
330-343
1003
HS-TEO
ST8
TRENT772B-60
THY06 0002
SIA04 0005
FIN02 0002
XLA01 0004
AVA01 0003
SIA04 0006
USA02 0001
SIA04 0007
FIN02 0003
AFL01 0003
330-243F
330-343
330-302
330-243
330-243
330-343
330-243
330-343
330-302
330-243
1004
1006
1007
1008
1009
1010
1011
1012
1013
1014
TC-JDO
C-GEGC
OH-LTN
4R-ALS
N968AV
OO-SFE
N279AY
C-GEGI
OH-LTO
VQ-BBE
ST9
ST8
ST8
ST7
ST7
ST8
ST7
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
SIA04 0008
AVA01 0004
SWR03 0002
51W01 0006
330-343
330-243
330-343
330-223
1015
1016
1018
1019
C-GEGP
N819CA
HB-JHB
VN-A378
ST8
ST7
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
68W01 0007
FWI02 0003
USA02 0002
FIN02 0004
EIN03 0003
SWR03 0004
68W01 0008
SWR03 0003
51W01 0007
ETD10 0002
78V01 0001
51W01 0008
THA07 0003
330-243
330-323
330-243
330-302
330-302
330-343
330-243
330-343
330-223
330-243F
330-243
330-223
330-343
1020
1021
1022
1023
1025
1026
1028
1029
1031
1032
1033
1034
1035
B-8019
EI-GOT
N280AY
OH-LTP
EI-EDY
HB-JHD
B-8550
HB-JHC
B-LNC
B-LDS
G-VYGE
B-LNI
HS-TEP
ST7
ST8
ST7
ST8
ST8
ST8
ST7
ST8
ST7
ST9
ST7
ST7
ST8
TRENT772B-60
PW4168A
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
ASY01 0004
330-203
1036
A39-004
ST7
CF6-80E1A3
THA07 0004
330-343
1037
HS-TEQ
ST8
TRENT772B-60
OMA02 0001
51W01 0009
USA02 0003
51W01 0010
AAW01 0003
OMA01 0001
AFL01 0004
330-243
330-223
330-243
330-223
330-202
330-343
330-243
1038
1039
1041
1042
1043
1044
1045
A4O-DA
B-LNE
N281AY
B-LND
5A-ONH
A4O-DB
VQ-BBF
ST7
ST7
ST7
ST7
ST7
ST8
ST7
TRENT772B-60
PW4168A
TRENT772B-60
PW4168A
CF6-80E1A4
TRENT772B-60
TRENT772B-60
78V01 0002
AFL01 0005
330-243
330-243
1046
1047
G-VYGA
VQ-BBG
ST7
ST7
TRENT772B-60
TRENT772B-60
XFA01 0003
OMA02 0002
68W02 0002
330-343
330-243
330-243F
1048
1049
1051
9M-XXC
A4O-DC
B-LNZ
ST8
ST7
ST9
TRENT772B-60
TRENT772B-60
TRENT772B-60
68W01 0009
97X02 0001
330-243
330-243
1052
1053
B-8221
VP-CAC
ST7
ST7
TRENT772B-60
TRENT772B-60
51W01 0011
AAR02 0002
330-223
330-323
1054
1055
B-LNG
HL7793
ST7
ST8
PW4168A
PW4168A
THAI AIRWAYS
INTERNATIONAL
TURKISH AIRLINES CO.
AIR CANADA
FINNAIR OYJ
SRILANKAN AIRLINES
AVIANCA S.A
BRUSSELS AIRLINES
AMERICAN AIRLINES, INC.
AIR CANADA
FINNAIR OYJ
AEROFLOT RUSSIAN
AIRLINES
AIR CANADA
NATIONAL AIRLINES
SWISS
ARCHWAY AVIATION
HOLDING
BEIJING CAPITAL AIRLINES
I FLY LTD
AMERICAN AIRLINES, INC.
FINNAIR OYJ
AER LINGUS LTD
SWISS
BEIJING CAPITAL AIRLINES
SWISS
HONG KONG AIRLINES LTD
AIR HONG KONG LTD
AIRTANKER SERVICES
HONG KONG AIRLINES LTD
THAI AIRWAYS
INTERNATIONAL
ROYAL AUSTRALIAN AIR
FORCE
THAI AIRWAYS
INTERNATIONAL
OMAN AIR
HONG KONG AIRLINES LTD
AMERICAN AIRLINES, INC.
HONG KONG AIRLINES LTD
AFRIQIYAH AIRWAYS
OMAN AIR
AEROFLOT RUSSIAN
AIRLINES
AIRTANKER SERVICES
AEROFLOT RUSSIAN
AIRLINES
AIRASIA X BERHAD
OMAN AIR
HONG KONG AIR CARGO
CARRIER
BEIJING CAPITAL AIRLINES
AMAC CORPORATE JET
AG
HONG KONG AIRLINES LTD
ASIANA AIRLINES, INC.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 14
MAINTENANCE PLANNING DOCUMENT
Version
Rank
MAU03 0002
AFL02 0001
51W01 0012
THA07 0005
Model
MSN
Registration
STD
Engine
Operator
330-202
330-343
330-223
330-343
1057
1058
1059
1060
3B-NBL
HS-XTK
B-LNF
HS-TER
ST7
ST8
ST7
ST8
CF6-80E1A4
TRENT772B-60
PW4168A
TRENT772B-60
QFA08 0001
68W02 0001
330-202
330-243F
1061
1062
VH-EBM
B-LNY
ST7
ST9
CF6-80E1A4
TRENT772B-60
OMA01 0002
AFL02 0002
XFA01 0004
FIN02 0005
USA02 0004
ETD10 0001
330-343
330-343
330-343
330-302
330-243
330-243F
1063
1065
1066
1067
1069
1070
A4O-DD
HS-XTL
9M-XXD
OH-LTR
N282AY
D-ALMD
ST8
ST8
ST8
ST8
ST7
ST9
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
ETD09 0001
AFL02 0003
AVA01 0005
THA07 0006
330-343
330-343
330-243
330-343
1071
1072
1073
1074
A6-AFA
HS-XTM
N973AV
HS-TES
ST8
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
XFA01 0005
USA02 0005
AFL02 0004
FIN02 0006
UAF01 0001
330-343
330-243
330-343
330-302
330-243
1075
1076
1077
1078
1080
9M-XXE
N283AY
F-HJAZ
OH-LTS
1300
ST8
ST7
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
ETD09 0002
CSC01 0001
SWR03 0005
SIA04 0009
THA07 0007
330-343
330-243
330-343
330-343
330-343
1081
1082
1084
1085
1086
A6-AFB
B-6518
HB-JHE
OO-SFX
HS-TET
ST8
ST7
ST8
ST8
ST8
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CCA04 0001
FIN02 0007
SWR03 0006
THA07 0008
330-343
330-302
330-343
330-343
1087
1088
1089
1090
B-6512
OH-LTT
HB-JHF
HS-TEU
ST8
ST8
ST8
ST8
TRENT772C-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
THY06 0001
OMA01 0003
QFA08 0002
USA02 0006
CSN03 0001
330-243F
330-343
330-202
330-243
330-223
1092
1093
1094
1095
1096
TC-JDP
A4O-DE
VH-EBN
N284AY
B-6135
ST9
ST8
ST7
ST7
ST7
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
PW4170
IWD01 0003
SIA04 0010
SIA04 0011
USA02 0007
SWR03 0007
AFL02 0005
HAL01 0001
SIA04 0012
EIN03 0004
SIA04 0013
330-343
330-343
330-343
330-243
330-343
330-343
330-243
330-343
330-302
330-343
1097
1098
1099
1100
1101
1103
1104
1105
1106
1107
EC-LXR
TC-LOL
B-LNR
N285AY
HB-JHG
F-HROK
N380HA
B-LNS
EI-ELA
D-ACVG
ST8
ST8
ST8
ST7
ST8
ST8
ST7
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
SVA01 0001
CCA04 0002
330-343
330-343
1108
1110
HZ-AQA
B-6511
ST8
ST8
TRENT772B-60
TRENT772C-60
AIR MAURITIUS
AIRASIA X BERHAD
HONG KONG AIRLINES LTD
THAI AIRWAYS
INTERNATIONAL
QANTAS AIRWAYS LTD.
HONG KONG AIR CARGO
CARRIER
OMAN AIR
AIRASIA X BERHAD
AIRASIA X BERHAD
FINNAIR OYJ
AMERICAN AIRLINES, INC.
EUROPEAN AIR
TRANSPORT
ETIHAD AIRWAYS
AIRASIA X BERHAD
AVIANCA S.A
THAI AIRWAYS
INTERNATIONAL
AIRASIA X BERHAD
AMERICAN AIRLINES, INC.
CORSAIR S.A.
FINNAIR OYJ
UNITED ARAB EMIRATES
AIR FORCE
ETIHAD AIRWAYS
SICHUAN AIRLINES
SWISS
BRUSSELS AIRLINES
THAI AIRWAYS
INTERNATIONAL
AIR CHINA LIMITED
FINNAIR OYJ
SWISS
THAI AIRWAYS
INTERNATIONAL
TURKISH AIRLINES CO.
OMAN AIR
QANTAS AIRWAYS LTD.
AMERICAN AIRLINES, INC.
CHINA SOUTHERN
AIRLINES
WORLD2FLY
TURKISH AIRLINES CO.
HONG KONG AIRLINES LTD
AMERICAN AIRLINES, INC.
SWISS
CORSAIR S.A.
HAWAIIAN AIRLINES, INC.
HONG KONG AIRLINES LTD
AER LINGUS LTD
EUROPEAN AIR
TRANSPORT
SAUDIA
AIR CHINA LIMITED
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 15
MAINTENANCE PLANNING DOCUMENT
Version
Rank
TAM03 0007
Model
MSN
Registration
STD
Engine
Operator
330-223
1112
9M-MTZ
ST7
PW4168A
HAL01 0002
68W02 0003
330-243
330-243F
1114
1115
N381HA
B-LNX
ST7
ST9
TRENT772B-60
TRENT772B-60
CSN03 0002
330-223
1116
B-6515
ST7
PW4170
TAM03 0008
OMA02 0003
AZA01 0001
SIA04 0014
XFA01 0006
SVA01 0002
CSN03 0003
330-223
330-243
330-202
330-343
330-343
330-343
330-223
1118
1120
1123
1124
1126
1127
1129
TC-JIZ
A4O-DF
EI-EJG
B-LDT
9M-XXF
HZ-AQB
B-6516
ST7
ST7
ST7
ST8
ST8
ST8
ST7
PW4168A
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
CCA04 0003
XFA01 0007
SIA04 0015
KAL05 0001
330-343
330-343
330-343
330-223
1130
1131
1132
1133
B-6513
9M-XXG
OO-SFF
HL8211
ST8
ST8
ST8
ST7
TRENT772C-60
TRENT772B-60
TRENT772B-60
PW4170
AZA01 0002
SVA01 0003
CSC01 0002
SVA01 0004
MSR04 0001
SWR03 0008
SIA04 0016
SVA01 0005
SIA04 0017
THY05 0001
AAR03 0001
SVA01 0006
KAL05 0002
330-202
330-343
330-243
330-343
330-343
330-343
330-343
330-343
330-343
330-343
330-323
330-343
330-223
1135
1137
1138
1141
1143
1145
1146
1147
1149
1150
1151
1153
1155
EI-EJH
HZ-AQC
B-6517
HZ-AQD
SU-GDS
HB-JHH
B-LHD
HZ-AQE
C-GKUG
TC-JNH
HL7794
HZ-AQF
HL8212
ST7
ST8
ST7
ST8
ST8
ST8
ST8
ST8
ST8
ST8
ST8
ST8
ST7
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4168A
TRENT772B-60
PW4170
SIA04 0018
SIA04 0019
68W01 0010
THY05 0002
KLM02 0001
330-343
330-343
330-243
330-343
330-203
1156
1157
1159
1160
1161
C-GKUH
OE-IEZ
B-6519
TC-JNI
PH-AOM
ST8
ST8
ST7
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
CPA08 0006
MAS03 0003
XFA01 0008
ETD09 0003
CRK01 0001
QFA09 0001
THY05 0003
HAL01 0003
THY05 0004
FIN02 0008
QFA09 0002
S2A01 0001
330-342
330-223F
330-343
330-343
330-343
330-202
330-343
330-243
330-343
330-302
330-202
330-243F
1163
1164
1165
1167
1168
1169
1170
1171
1172
1173
1174
1175
B-LAJ
TC-JOO
9M-XXH
A6-AFC
B-6520
VH-EBO
TC-JNJ
N382HA
TC-JNK
OH-LTU
VH-EBP
B-LNV
ST8
ST9
ST8
ST8
ST8
ST7
ST8
ST7
ST8
ST8
ST7
ST9
TRENT772-60
PW4170
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
CAL03 0018
CRK01 0002
330-302
330-343
1177
1178
B-18355
B-6527
ST8
ST8
CF6-80E1A4
TRENT772B-60
MALAYSIA AIRLINES
BERHAD
HAWAIIAN AIRLINES, INC.
HONG KONG AIR CARGO
CARRIER
CHINA SOUTHERN
AIRLINES
TURKISH AIRLINES CO.
OMAN AIR
ALITALIA
AIR HONG KONG LTD
AIRASIA X BERHAD
SAUDIA
CHINA SOUTHERN
AIRLINES
AIR CHINA LIMITED
AIRASIA X BERHAD
BRUSSELS AIRLINES
KOREAN AIR LINES CO.
LTD
ALITALIA
SAUDIA
SICHUAN AIRLINES
SAUDIA
EGYPTAIR
SWISS
HONG KONG AIRLINES LTD
SAUDIA
AIR CANADA
TURKISH AIRLINES CO.
ASIANA AIRLINES, INC.
SAUDIA
KOREAN AIR LINES CO.
LTD
AIR CANADA
AIR GEORGIA LLC
HAINAN AIRLINES
TURKISH AIRLINES CO.
KLM ROYAL DUTCH
AIRLINES
CATHAY PACIFIC
TURKISH AIRLINES CO.
AIRASIA X BERHAD
ETIHAD AIRWAYS
HAINAN AIRLINES
QANTAS AIRWAYS LTD.
TURKISH AIRLINES CO.
HAWAIIAN AIRLINES, INC.
TURKISH AIRLINES CO.
FINNAIR OYJ
QANTAS AIRWAYS LTD.
HONG KONG AIR CARGO
CARRIER
CHINA AIRLINES LTD
HAINAN AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 16
MAINTENANCE PLANNING DOCUMENT
Version
Rank
MAS03 0004
Model
MSN
Registration
STD
Engine
Operator
330-223F
1180
9M-MUD
ST9
PW4170
SWR03 0009
ASY01 0005
330-343
330-203
1181
1183
HB-JHI
A39-005
ST8
ST7
TRENT772B-60
CF6-80E1A3
68W01 0011
UAF01 0002
330-243
330-243
1184
1186
PK-GPL
1301
ST7
ST7
TRENT772B-60
TRENT772B-60
CCA05 0001
SWR03 0010
SVA01 0007
CRK01 0003
SAA03 0001
SVA01 0008
EDW02 0001
VIR09 0001
CPA09 0001
QFA10 0001
CCA05 0002
KAL05 0003
330-343
330-343
330-343
330-343
330-243
330-343
330-343
330-343
330-343
330-202
330-343
330-223
1187
1188
1189
1190
1191
1192
1193
1195
1196
1198
1199
1200
B-6523
HB-JHJ
HZ-AQH
B-6529
ZS-SXZ
HZ-AQG
D-AFYQ
G-VSXY
B-LAK
VH-EBQ
B-6525
HL8227
ST8
ST8
ST8
ST8
ST7
ST8
ST8
ST8
ST8
ST7
ST8
ST7
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772C-60
PW4170
VIR09 0002
CSN03 0004
330-343
330-223
1201
1202
G-VKSS
B-6528
ST8
ST7
TRENT772B-60
PW4170
KAL05 0004
330-223
1203
HL8228
ST7
PW4170
THY05 0005
ETD11 0001
VIR09 0003
AVA01 0006
MAS02 0001
330-343
330-343
330-343
330-243
330-323
1204
1205
1206
1208
1209
TC-JNL
A6-AFD
G-VLUV
N974AV
9M-MTA
ST8
ST8
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
SAA03 0002
AAR03 0002
THY05 0006
TAM03 0009
GIA02 0001
VIR09 0004
CCA05 0003
HAL01 0004
AZA01 0003
MAS02 0002
330-243
330-323
330-343
330-223
330-243
330-343
330-343
330-243
330-202
330-323
1210
1211
1212
1213
1214
1215
1216
1217
1218
1219
EC-NOE
HL7795
TC-JNM
TC-LOH
PK-GPM
G-VGEM
B-6530
N383HA
EI-EJI
9M-MTB
ST7
ST8
ST8
ST7
ST7
ST8
ST8
ST7
ST7
ST8
TRENT772B-60
PW4168A
TRENT772B-60
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
PW4170
CSN03 0005
330-223
1220
B-6526
ST7
PW4170
TAM03 0010
CPA09 0002
SAA03 0003
AVA01 0007
AZA01 0004
ETD11 0002
OMA02 0004
THY05 0007
MAS02 0003
330-223
330-343
330-243
330-243
330-202
330-343
330-243
330-343
330-323
1221
1222
1223
1224
1225
1226
1227
1228
1229
TC-LOI
B-LAL
ZS-SXX
N975AV
EI-EJJ
A6-AFE
A4O-DG
TC-JNN
9M-MTC
ST7
ST8
ST7
ST7
ST7
ST8
ST7
ST8
ST8
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
MSR04 0002
330-343
1230
SU-GDT
ST8
TRENT772B-60
MALAYSIA AIRLINES
BERHAD
SWISS
ROYAL AUSTRALIAN AIR
FORCE
GARUDA INDONESIA
UNITED ARAB EMIRATES
AIR FORCE
AIR CHINA LIMITED
SWISS
SAUDIA
HAINAN AIRLINES
AIRCASTLE ADVISOR LLC
SAUDIA
EW DISCOVER GMBH
VIRGIN ATLANTIC
CATHAY PACIFIC
QANTAS AIRWAYS LTD.
AIR CHINA LIMITED
KOREAN AIR LINES CO.
LTD
VIRGIN ATLANTIC
CHINA SOUTHERN
AIRLINES
KOREAN AIR LINES CO.
LTD
TURKISH AIRLINES CO.
ETIHAD AIRWAYS
VIRGIN ATLANTIC
AVIANCA S.A
MALAYSIA AIRLINES
BERHAD
AURA AIRLINES SL
ASIANA AIRLINES, INC.
TURKISH AIRLINES CO.
TURKISH AIRLINES CO.
GARUDA INDONESIA
VIRGIN ATLANTIC
AIR CHINA LIMITED
HAWAIIAN AIRLINES, INC.
ALITALIA
MALAYSIA AIRLINES
BERHAD
CHINA SOUTHERN
AIRLINES
TURKISH AIRLINES CO.
CATHAY PACIFIC
AIRCASTLE ADVISOR LLC
AVIANCA S.A
ALITALIA
ETIHAD AIRWAYS
OMAN AIR
TURKISH AIRLINES CO.
MALAYSIA AIRLINES
BERHAD
EGYPTAIR
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 17
MAINTENANCE PLANNING DOCUMENT
Version
Rank
VIR09 0005
AFL02 0006
Model
MSN
Registration
STD
Engine
Operator
330-343
330-343
1231
1232
G-VINE
VQ-BQX
ST8
ST8
TRENT772B-60
TRENT772B-60
CSN03 0006
330-223
1233
B-6531
ST7
PW4170
MAS02 0004
330-323
1234
9M-MTD
ST8
PW4170
RSF01 0003
SAA03 0004
CCA06 0001
MSR04 0003
CPA09 0003
THY07 0001
CSC01 0003
MAS02 0005
330-202
330-243
330-243
330-343
330-343
330-243
330-243
330-323
1235
1236
1237
1238
1239
1240
1241
1243
2403
ZS-SXW
B-6533
SU-GDU
B-LAM
TC-TUR
B-6535
9M-MTE
ST7
ST7
ST7
ST8
ST8
ST7
ST7
ST8
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
PW4170
CSN03 0007
330-223
1244
B-6532
ST7
PW4170
ETD11 0003
MSR04 0004
AFL02 0007
330-343
330-343
330-343
1245
1246
1247
A6-AFF
SU-GDV
VQ-BQY
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
78V01 0003
SAA03 0005
330-243
330-243
1248
1249
G-VYGB
ZS-SXV
ST7
ST7
TRENT772B-60
TRENT772B-60
UAF01 0003
330-243
1250
1302
ST7
TRENT772B-60
QFA10 0002
AZA01 0005
EVA03 0001
330-202
330-202
330-302
1251
1252
1254
VH-EBR
EI-EJK
B-16331
ST7
ST7
ST8
CF6-80E1A4
CF6-80E1A4
CF6-80E1A4
CRK01 0004
HVN01 0001
QFA10 0003
HAL01 0005
CCA06 0002
GIA02 0002
CES05 0001
THA08 0001
330-343
330-223
330-202
330-243
330-243
330-243
330-243
330-343
1255
1256
1258
1259
1260
1261
1262
1263
B-6539
VP-BUQ
VH-EBS
N384HA
B-6536
PK-GPN
B-6537
HS-TBA
ST8
ST7
ST7
ST7
ST7
ST7
ST7
ST8
TRENT772C-60
PW4168A
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
MSR04 0005
330-343
1264
VQ-BNS
ST8
TRENT772B-60
FWI02 0004
HVN01 0002
CES05 0002
EVA03 0002
330-323
330-223
330-243
330-302
1265
1266
1267
1268
F-HPTP
VP-BUT
B-6538
B-16332
ST8
ST7
ST7
ST8
PW4168A
PW4168A
TRENT772C-60
CF6-80E1A4
THA08 0002
330-343
1269
HS-TBB
ST8
TRENT772B-60
AFL02 0008
330-343
1270
VQ-BQZ
ST8
TRENT772B-60
SAA03 0006
CAL04 0001
EVA03 0003
330-243
330-302
330-302
1271
1272
1274
ZS-SXU
B-18356
B-16333
ST7
ST8
ST8
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
78V01 0004
SWR04 0001
330-243
330-343
1275
1276
G-VYGC
HB-JHK
ST7
ST8
TRENT772B-60
TRENT772B-60
VIRGIN ATLANTIC
AEROFLOT RUSSIAN
AIRLINES
CHINA SOUTHERN
AIRLINES
MALAYSIA AIRLINES
BERHAD
ROYAL SAUDI AIR FORCE
AIRCASTLE ADVISOR LLC
AIR CHINA LIMITED
EGYPTAIR
CATHAY PACIFIC
TURKISH AIRLINES CO.
SICHUAN AIRLINES
MALAYSIA AIRLINES
BERHAD
CHINA SOUTHERN
AIRLINES
ETIHAD AIRWAYS
EGYPTAIR
AEROFLOT RUSSIAN
AIRLINES
AIRTANKER SERVICES
AVIATION CAPITAL GROUP
LLC
UNITED ARAB EMIRATES
AIR FORCE
QANTAS AIRWAYS LTD.
ALITALIA
EVA AIRWAYS
CORPORATION
HAINAN AIRLINES
NORDWIND AIRLINES
QANTAS AIRWAYS LTD.
HAWAIIAN AIRLINES, INC.
AIR CHINA LIMITED
GARUDA INDONESIA
CHINA EASTERN AIRLINES
THAI AIRWAYS
INTERNATIONAL
AEROFLOT RUSSIAN
AIRLINES
I FLY LTD
AIR LEASE CORPORATION
CHINA EASTERN AIRLINES
EVA AIRWAYS
CORPORATION
THAI AIRWAYS
INTERNATIONAL
AEROFLOT RUSSIAN
AIRLINES
SOUTH AFRICAN AIRWAYS
CHINA AIRLINES LTD
EVA AIRWAYS
CORPORATION
AIRTANKER SERVICES
SWISS
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 18
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CRK02 0001
CAL04 0002
AVA01 0008
CES05 0003
MAS02 0006
Model
MSN
Registration
STD
Engine
Operator
330-243
330-302
330-243
330-243
330-323
1277
1278
1279
1280
1281
B-30EM
B-18357
N279AV
B-6543
9M-MTF
ST7
ST8
ST7
ST7
ST8
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
PW4170
CCA06 0003
AZA01 0006
AFL02 0009
330-243
330-202
330-343
1282
1283
1284
B-6540
EI-EJL
VQ-BMV
ST7
ST7
ST8
TRENT772C-60
CF6-80E1A4
TRENT772B-60
CPA10 0001
CRK02 0002
KLM03 0001
330-343
330-243
330-303
1285
1286
1287
B-LAN
B-30EN
PH-AKA
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
CF6-80E1A3
GIA02 0003
THA08 0003
330-243
330-343
1288
1289
PK-GPO
HS-TBC
ST7
ST8
TRENT772B-60
TRENT772B-60
SWR04 0002
CES05 0004
DLH10 0001
330-343
330-243
330-343
1290
1291
1292
HB-JHL
B-6545
D-AIKP
ST8
ST7
ST8
TRENT772B-60
TRENT772C-60
TRENT772B-60
VOZ01 0001
330-243
1293
VH-XFC
ST7
TRENT772B-60
KLM03 0002
330-303
1294
PH-AKB
ST8
CF6-80E1A3
HAL01 0006
VIR08 0001
CSN03 0008
330-243
330-343
330-223
1295
1296
1297
N385HA
G-VRAY
B-6542
ST7
ST8
ST7
TRENT772B-60
TRENT772B-60
PW4170
THY05 0008
AFL02 0010
330-343
330-343
1298
1299
TC-JNO
VQ-BMX
ST8
ST8
TRENT772B-60
TRENT772B-60
KLM03 0003
330-303
1300
PH-AKD
ST8
CF6-80E1A3
AFL02 0011
330-343
1301
VQ-BMY
ST8
TRENT772B-60
HAL01 0007
CES05 0005
CCA06 0004
DLH10 0002
330-243
330-243
330-243
330-343
1302
1303
1304
1305
N386HA
B-6546
B-6541
D-AIKQ
ST7
ST7
ST7
ST8
TRENT772B-60
TRENT772C-60
TRENT772C-60
TRENT772B-60
VOZ01 0002
THY05 0009
AZA01 0007
CSN03 0009
330-243
330-343
330-202
330-223
1306
1307
1308
1309
VH-XFD
TC-JNP
EI-EJM
B-6547
ST7
ST8
ST7
ST7
TRENT772B-60
TRENT772B-60
CF6-80E1A4
PW4170
HAL01 0008
THY05 0010
78V01 0005
AZA01 0008
DLH10 0003
330-243
330-343
330-243
330-202
330-343
1310
1311
1312
1313
1314
N388HA
TC-JNR
G-VYGD
EI-EJN
D-AIKR
ST7
ST8
ST7
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
VIR08 0002
HAL01 0009
CPA10 0002
MAS02 0007
330-343
330-243
330-343
330-323
1315
1316
1317
1318
G-VNYC
N389HA
B-LAO
9M-MTG
ST8
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
TIANJIN AIRLINES CO. LTD
CHINA AIRLINES LTD
AVIANCA S.A
CHINA EASTERN AIRLINES
MALAYSIA AIRLINES
BERHAD
AIR CHINA LIMITED
ALITALIA
AEROFLOT RUSSIAN
AIRLINES
CATHAY PACIFIC
TIANJIN AIRLINES CO. LTD
KLM ROYAL DUTCH
AIRLINES
GARUDA INDONESIA
THAI AIRWAYS
INTERNATIONAL
SWISS
CHINA EASTERN AIRLINES
DEUTSCHE LUFTHANSA
AG
GLOBAL KNAFAIM
LEASING LTD
KLM ROYAL DUTCH
AIRLINES
HAWAIIAN AIRLINES, INC.
VIRGIN ATLANTIC
CHINA SOUTHERN
AIRLINES
TURKISH AIRLINES CO.
AEROFLOT RUSSIAN
AIRLINES
KLM ROYAL DUTCH
AIRLINES
AEROFLOT RUSSIAN
AIRLINES
HAWAIIAN AIRLINES, INC.
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
DEUTSCHE LUFTHANSA
AG
ORIX CORPORATION
TURKISH AIRLINES CO.
ALITALIA
CHINA SOUTHERN
AIRLINES
HAWAIIAN AIRLINES, INC.
TURKISH AIRLINES CO.
AIRTANKER SERVICES
ALITALIA
DEUTSCHE LUFTHANSA
AG
VIRGIN ATLANTIC
HAWAIIAN AIRLINES, INC.
CATHAY PACIFIC
MALAYSIA AIRLINES
BERHAD
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 19
MAINTENANCE PLANNING DOCUMENT
Version
Rank
VOZ01 0003
S2A01 0002
Model
MSN
Registration
STD
Engine
Operator
330-243
330-243F
1319
1320
VH-XFE
B-LNW
ST7
ST9
TRENT772B-60
TRENT772B-60
XAX02 0001
CRK02 0003
AFL02 0012
330-202
330-243
330-343
1321
1322
1323
VP-CKQ
B-LNL
VQ-BPI
ST7
ST7
ST8
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CES05 0006
CRK01 0005
AAR03 0003
AZA01 0009
AFL02 0013
330-243
330-343
330-323
330-202
330-343
1324
1325
1326
1327
1328
B-5902
B-5905
HL8258
EI-EJO
VQ-BPJ
ST7
ST8
ST8
ST7
ST8
TRENT772C-60
TRENT772B-60
PW4168A
CF6-80E1A4
TRENT772B-60
VIR08 0003
CCA06 0005
CES05 0007
MNB02 0001
CCA07 0001
78V01 0006
CSN03 0010
330-343
330-243
330-243
330-243F
330-343
330-243
330-223
1329
1330
1331
1332
1333
1334
1335
G-VGBR
B-6549
B-5903
TC-MCZ
B-6503
G-VYGF
B-6548
ST8
ST7
ST7
ST9
ST8
ST7
ST7
TRENT772B-60
TRENT772C-60
TRENT772C-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
PW4170
MAS02 0008
330-323
1336
9M-MTH
ST8
PW4170
MAS02 0009
330-323
1337
9M-MTI
ST8
PW4170
THA08 0004
330-343
1338
HS-TBD
ST8
TRENT772B-60
XAX02 0002
AAR03 0004
VIR08 0004
AVA01 0009
CPA10 0003
THY06 0003
AFL02 0014
330-202
330-323
330-343
330-243
330-343
330-243F
330-343
1339
1340
1341
1342
1343
1344
1345
YI-AQY
HL8259
G-VWAG
N342AV
B-LAP
TC-JDR
VQ-BPK
ST7
ST8
ST8
ST7
ST8
ST9
ST8
CF6-80E1A4
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CAL04 0003
MAS02 0010
330-302
330-323
1346
1347
B-18358
9M-MTJ
ST8
ST8
CF6-80E1A4
PW4170
THA08 0005
330-343
1348
HS-TBE
ST8
TRENT772B-60
CPA10 0004
S2A01 0003
JAI03 0001
VIR08 0005
CCA07 0002
AZA01 0010
SWR04 0003
AFL02 0015
330-343
330-243F
330-302
330-343
330-343
330-202
330-343
330-343
1349
1350
1351
1352
1353
1354
1355
1356
B-LAQ
B-308L
VP-BUH
G-VUFO
B-5901
EI-EJP
HB-JHM
VP-BDD
ST8
ST9
ST8
ST8
ST8
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TNA01 0001
CRK01 0006
CRL03 0001
XLF01 0001
JAI03 0002
CPA10 0005
78V01 0007
330-343
330-343
330-343
330-303
330-302
330-343
330-243
1357
1358
1359
1360
1361
1362
1363
N803AV
B-LNM
F-HSKY
VP-BUI
VP-BUM
B-LAR
G-VYGG
ST8
ST8
ST8
ST8
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
TRENT772B-60
TRENT772B-60
ORIX CORPORATION
HONG KONG AIR CARGO
CARRIER
AEGLE AVIATION
TIANJIN AIRLINES CO. LTD
AEROFLOT RUSSIAN
AIRLINES
CHINA EASTERN AIRLINES
HAINAN AIRLINES
ASIANA AIRLINES, INC.
ALITALIA
AEROFLOT RUSSIAN
AIRLINES
VIRGIN ATLANTIC
AIR CHINA LIMITED
CHINA EASTERN AIRLINES
MNG AIRLINES
AIR CHINA LIMITED
AIRTANKER SERVICES
CHINA SOUTHERN
AIRLINES
MALAYSIA AIRLINES
BERHAD
MALAYSIA AIRLINES
BERHAD
THAI AIRWAYS
INTERNATIONAL
IRAQI AIRWAYS
ASIANA AIRLINES, INC.
VIRGIN ATLANTIC
AVIANCA S.A
CATHAY PACIFIC
TURKISH AIRLINES CO.
AEROFLOT RUSSIAN
AIRLINES
CHINA AIRLINES LTD
MALAYSIA AIRLINES
BERHAD
THAI AIRWAYS
INTERNATIONAL
CATHAY PACIFIC
SICHUAN AIRLINES
NORDWIND AIRLINES
VIRGIN ATLANTIC
AIR CHINA LIMITED
ALITALIA
SWISS
AEROFLOT RUSSIAN
AIRLINES
DEUCALION AVIATION LTD
HONG KONG AIRLINES LTD
CORSAIR S.A.
NORDWIND AIRLINES
NORDWIND AIRLINES
CATHAY PACIFIC
AIRTANKER SERVICES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 20
MAINTENANCE PLANNING DOCUMENT
Version
Rank
GIA02 0004
QFA09 0003
CPA10 0006
CAL04 0004
TPA01 0001
CRK01 0007
JAI03 0003
AFL02 0016
Model
MSN
Registration
STD
Engine
Operator
330-243
330-202
330-343
330-302
330-243F
330-343
330-302
330-343
1364
1365
1366
1367
1368
1369
1370
1371
PK-GPP
VH-EBV
B-LAX
B-18359
N330QT
B-LNN
VP-BUP
VP-BDE
ST7
ST7
ST8
ST8
ST9
ST8
ST8
ST8
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CES05 0008
CCA07 0003
THA08 0006
330-243
330-343
330-343
1372
1373
1374
B-5908
B-5906
HS-TBF
ST7
ST8
ST8
TRENT772C-60
TRENT772C-60
TRENT772B-60
CES05 0009
CRL03 0002
IBE08 0001
TNA01 0002
RSF01 0004
TPA01 0002
KLM03 0004
330-243
330-343
330-302
330-343
330-202
330-243F
330-303
1375
1376
1377
1378
1379
1380
1381
B-5920
F-HZEN
EC-LUB
N804AV
2404
N331QT
PH-AKE
ST7
ST8
ST8
ST8
ST7
ST9
ST8
TRENT772C-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A3
SIA05 0001
330-343
1382
9H-SMD
ST8
TRENT772B-60
CCA07 0004
CRK01 0008
IBE08 0002
S2A01 0004
CPA10 0007
MAS02 0011
330-343
330-343
330-302
330-243F
330-343
330-323
1383
1384
1385
1386
1387
1388
B-5916
B-LNO
EC-LUK
B-308P
B-LAZ
9M-MTK
ST8
ST8
ST8
ST9
ST8
ST8
TRENT772C-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
PW4170
HAL01 0010
78V01 0008
JAI03 0004
330-243
330-243
330-302
1389
1390
1391
N390HA
G-VYGH
VP-BUJ
ST7
ST7
ST8
TRENT772B-60
TRENT772B-60
CF6-80E1A4
CSN04 0001
330-323
1392
B-5917
ST8
PW4170
KAL05 0005
330-223
1393
HL8276
ST7
PW4170
FJI01 0001
MAS02 0012
330-243
330-323
1394
1395
DQ-FJT
9M-MTL
ST7
ST8
TRENT772B-60
PW4170
CCA06 0006
CSC02 0001
CRK01 0009
HAL01 0011
AVA01 0010
SIA05 0002
CES05 0010
SWR04 0004
HAL01 0012
IBE08 0003
S2A01 0005
VOZ01 0004
THA08 0007
330-243
330-343
330-343
330-243
330-243
330-343
330-243
330-343
330-243
330-302
330-243F
330-243
330-343
1396
1397
1398
1399
1400
1401
1402
1403
1404
1405
1406
1407
1408
B-5918
B-5923
B-LNP
N391HA
N280AV
9H-HFC
B-5921
HB-JHN
N392HA
EC-LUX
B-308Q
VH-XFG
HS-TBG
ST7
ST8
ST8
ST7
ST7
ST8
ST7
ST8
ST7
ST8
ST9
ST7
ST8
TRENT772C-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
CPA10 0008
330-343
1409
B-LBA
ST8
TRENT772B-60
GARUDA INDONESIA
QANTAS AIRWAYS LTD.
CATHAY PACIFIC
CHINA AIRLINES LTD
AVIANCA CARGO
HONG KONG AIRLINES LTD
NORDWIND AIRLINES
AEROFLOT RUSSIAN
AIRLINES
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
THAI AIRWAYS
INTERNATIONAL
CHINA EASTERN AIRLINES
CORSAIR S.A.
IBERIA
DEUCALION AVIATION LTD
ROYAL SAUDI AIR FORCE
AVIANCA CARGO
KLM ROYAL DUTCH
AIRLINES
SMARTLYNX AIRLINES
MALTA
AIR CHINA LIMITED
HONG KONG AIRLINES LTD
IBERIA
SICHUAN AIRLINES
CATHAY PACIFIC
MALAYSIA AIRLINES
BERHAD
HAWAIIAN AIRLINES, INC.
AIRTANKER SERVICES
GE CAPITAL AVIATION
SERVICES
CHINA SOUTHERN
AIRLINES
KOREAN AIR LINES CO.
LTD
AIR PACIFIC LIMITED
MALAYSIA AIRLINES
BERHAD
AIR CHINA LIMITED
SICHUAN AIRLINES
HONG KONG AIRLINES LTD
HAWAIIAN AIRLINES, INC.
AVIANCA S.A
MERCED CAPITAL L.P
CHINA EASTERN AIRLINES
SWISS
HAWAIIAN AIRLINES, INC.
IBERIA
SICHUAN AIRLINES
DORIC GMBH
THAI AIRWAYS
INTERNATIONAL
CATHAY PACIFIC
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 21
MAINTENANCE PLANNING DOCUMENT
Version
Rank
GIA02 0005
XFA01 0009
LAA01 0001
CCA07 0005
ETD12 0001
USA02 0008
FJI01 0002
USA02 0009
THY06 0004
78V01 0009
CEB01 0001
CES05 0011
HAL01 0013
XFA01 0010
CSN04 0002
Model
MSN
Registration
STD
Engine
Operator
330-243
330-343
330-202
330-343
330-243F
330-243
330-243
330-243
330-243F
330-243
330-343
330-243
330-243
330-343
330-323
1410
1411
1412
1413
1414
1415
1416
1417
1418
1419
1420
1421
1422
1423
1425
PK-GPQ
9M-XXI
5A-LAR
B-5919
B-LDP
N286AY
DQ-FJU
N287AY
TC-JDS
G-VYGI
RP-C3341
B-5926
N393HA
9M-XXJ
B-5922
ST7
ST8
ST7
ST8
ST9
ST7
ST7
ST7
ST9
ST7
ST8
ST7
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
PW4170
IBE08 0004
SIA05 0003
TPA01 0003
CES05 0012
CSN04 0003
330-302
330-343
330-243F
330-243
330-323
1426
1427
1428
1429
1430
EC-LXK
A4O-DZ
N332QT
B-5930
B-5928
ST8
ST8
ST9
ST7
ST8
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772C-60
PW4170
MAS02 0013
330-323
1431
9M-MTM
ST8
PW4170
CSC02 0002
XFA01 0011
CCA06 0007
AAR03 0005
CPA10 0009
IBE08 0005
CRK01 0010
78V01 0010
CES05 0013
USA02 0010
THY06 0005
CPA10 0010
CCA06 0008
CEB01 0002
GIA03 0001
SIA05 0004
TPA01 0004
PAL04 0001
CAL04 0005
NMB01 0001
VOZ01 0005
SIA05 0005
SVA02 0001
USA02 0011
PAL04 0002
HDA07 0001
THY08 0001
CCA06 0009
PAL04 0003
CES05 0014
SVA02 0002
330-343
330-343
330-243
330-323
330-343
330-302
330-343
330-243
330-243
330-243
330-243F
330-343
330-243
330-343
330-343
330-343
330-243F
330-343
330-302
330-243
330-243
330-343
330-343
330-243
330-343
330-343
330-303
330-243
330-343
330-243
330-343
1432
1433
1434
1435
1436
1437
1438
1439
1440
1441
1442
1443
1444
1445
1446
1447
1448
1449
1450
1451
1452
1453
1454
1455
1456
1457
1458
1459
1460
1461
1462
B-5929
9M-XXK
B-5925
HL8282
B-LBB
EC-LYF
B-5935
G-VYGJ
B-5931
N288AY
TC-JCI
B-LBC
B-5927
RP-C3342
PK-GPR
9V-STW
N334QT
RP-C8782
B-18360
V5-ANO
VH-XFH
9H-TAJ
HZ-AQI
N289AY
RP-C8780
B-HWM
TC-JNS
B-5932
RP-C8781
B-5936
HZ-AQK
ST8
ST8
ST7
ST8
ST8
ST8
ST8
ST7
ST7
ST7
ST9
ST8
ST7
ST8
ST8
ST8
ST9
ST8
ST8
ST7
ST7
ST8
ST8
ST7
ST8
ST8
ST8
ST7
ST8
ST7
ST8
TRENT772C-60
TRENT772B-60
TRENT772C-60
PW4168A
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772C-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
GARUDA INDONESIA
AIRASIA X BERHAD
LIBYAN AIRLINES
AIR CHINA LIMITED
AIR HONG KONG LTD
AMERICAN AIRLINES, INC.
AIR PACIFIC LIMITED
AMERICAN AIRLINES, INC.
TURKISH AIRLINES CO.
AIRTANKER SERVICES
CEBU AIR, INC
CHINA EASTERN AIRLINES
HAWAIIAN AIRLINES, INC.
AIRASIA X BERHAD
CHINA SOUTHERN
AIRLINES
IBERIA
FPG AMENTUM LIMITED
AVIANCA CARGO
CHINA EASTERN AIRLINES
CHINA SOUTHERN
AIRLINES
MALAYSIA AIRLINES
BERHAD
SICHUAN AIRLINES
SERAPH AVIATION
AIR CHINA LIMITED
ASIANA AIRLINES, INC.
CATHAY PACIFIC
IBERIA
HAINAN AIRLINES
AIRTANKER SERVICES
CHINA EASTERN AIRLINES
AMERICAN AIRLINES, INC.
TURKISH AIRLINES CO.
CATHAY PACIFIC
AIR CHINA LIMITED
CEBU AIR, INC
GARUDA INDONESIA
SERAPH AVIATION
AVIANCA CARGO
PHILIPPINE AIRLINES, INC.
CHINA AIRLINES LTD
AIR NAMIBIA
AVOLON
HI FLY MALTA
SAUDIA
AMERICAN AIRLINES, INC.
PHILIPPINE AIRLINES, INC.
CATHAY PACIFIC
TURKISH AIRLINES CO.
AIR CHINA LIMITED
PHILIPPINE AIRLINES, INC.
CHINA EASTERN AIRLINES
SAUDIA
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 22
MAINTENANCE PLANNING DOCUMENT
Version
Rank
PAL04 0004
AAR03 0006
FJI01 0003
NMB01 0002
PAL04 0005
CES05 0015
HAL01 0014
MAS02 0014
Model
MSN
Registration
STD
Engine
Operator
330-343
330-323
330-243
330-243
330-343
330-243
330-243
330-323
1463
1464
1465
1466
1467
1468
1469
1470
RP-C8783
HL8286
DQ-FJV
V5-ANP
RP-C8784
B-5937
N395HA
9M-MTN
ST8
ST8
ST7
ST7
ST8
ST7
ST7
ST8
TRENT772B-60
PW4168A
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
PW4170
CCA06 0010
AAW02 0001
SVA02 0003
GIA02 0006
PAL04 0006
THY08 0002
SIA05 0006
330-243
330-202
330-343
330-243
330-343
330-303
330-343
1471
1472
1473
1474
1475
1476
1477
B-5933
5A-ONP
HZ-AQJ
PK-GPS
RP-C8785
TC-JNT
D-AJFK
ST7
ST7
ST8
ST7
ST8
ST8
ST8
TRENT772C-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772B-60
RSF01 0005
CES05 0016
USA02 0012
XFA01 0012
PAL04 0007
SKY01 0001
CES06 0001
SIA05 0007
ETD13 0001
THY08 0003
HAL01 0015
MAS02 0015
330-202
330-243
330-243
330-343
330-343
330-343
330-243
330-343
330-243
330-303
330-243
330-323
1478
1479
1480
1481
1482
1483
1484
1485
1486
1487
1488
1489
2405
B-5938
N290AY
9M-XXP
RP-C8786
TC-LOA
B-5941
C-GOFW
A6-EYT
TC-JNZ
N396HA
9M-MTO
ST7
ST7
ST7
ST8
ST8
ST8
ST7
ST8
ST7
ST8
ST7
ST8
CF6-80E1A4
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772B-60
PW4170
IBE08 0006
SKY01 0002
ONE02 0001
CCA07 0006
CSN04 0004
330-302
330-343
330-243
330-343
330-323
1490
1491
1492
1493
1494
EC-LZJ
TC-LOB
PR-AIS
B-5912
B-5939
ST8
ST8
ST7
ST8
ST8
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772C-60
PW4170
CEB01 0003
HAL01 0016
DLH10 0004
330-343
330-243
330-343
1495
1496
1497
RP-C3343
N399HA
D-AIKS
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
78V01 0011
AAW03 0001
CES06 0002
THY08 0004
USA02 0013
CPA11 0001
PAL04 0008
LAA01 0003
ONE01 0001
IBE08 0007
ONE02 0002
CCA07 0007
PAL05 0001
HAL01 0017
USA02 0014
SVA02 0004
330-243
330-302
330-243
330-303
330-243
330-343
330-343
330-202
330-243F
330-302
330-243
330-343
330-343
330-243
330-243
330-343
1498
1499
1500
1501
1502
1503
1504
1505
1506
1507
1508
1509
1510
1511
1512
1513
G-VYGK
TC-JOM
B-5942
TC-JOA
N291AY
B-LBD
RP-C8789
5A-LAT
N336QT
EC-LZX
G-POWX
B-5913
RP-C8760
N370HA
N292AY
HZ-AQL
ST7
ST8
ST7
ST8
ST7
ST8
ST8
ST7
ST9
ST8
ST7
ST8
ST8
ST7
ST7
ST8
TRENT772B-60
CF6-80E1A4
TRENT772C-60
CF6-80E1A3
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PHILIPPINE AIRLINES, INC.
ASIANA AIRLINES, INC.
AIR PACIFIC LIMITED
AIR NAMIBIA
PHILIPPINE AIRLINES, INC.
CHINA EASTERN AIRLINES
HAWAIIAN AIRLINES, INC.
MALAYSIA AIRLINES
BERHAD
AIR CHINA LIMITED
AFRIQIYAH AIRWAYS
SAUDIA
GARUDA INDONESIA
PHILIPPINE AIRLINES, INC.
TURKISH AIRLINES CO.
EUROPEAN AIR
TRANSPORT
ROYAL SAUDI AIR FORCE
CHINA EASTERN AIRLINES
AMERICAN AIRLINES, INC.
AIRASIA X BERHAD
PHILIPPINE AIRLINES, INC.
TURKISH AIRLINES CO.
CHINA EASTERN AIRLINES
AIR CANADA
ETIHAD AIRWAYS
TURKISH AIRLINES CO.
HAWAIIAN AIRLINES, INC.
MALAYSIA AIRLINES
BERHAD
IBERIA
TURKISH AIRLINES CO.
AZUL
AIR CHINA LIMITED
CHINA SOUTHERN
AIRLINES
CEBU AIR, INC
HAWAIIAN AIRLINES, INC.
DEUTSCHE LUFTHANSA
AG
AIRTANKER SERVICES
TURKISH AIRLINES CO.
CHINA EASTERN AIRLINES
TURKISH AIRLINES CO.
AMERICAN AIRLINES, INC.
CATHAY PACIFIC
PHILIPPINE AIRLINES, INC.
LIBYAN AIRLINES
AVIANCA CARGO
IBERIA
AVOLON
AIR CHINA LIMITED
PHILIPPINE AIRLINES, INC.
HAWAIIAN AIRLINES, INC.
AMERICAN AIRLINES, INC.
SAUDIA
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 23
MAINTENANCE PLANNING DOCUMENT
Version
Rank
THY08 0005
IBE08 0008
RSF01 0006
SIA05 0008
AAR03 0007
CSN04 0005
Model
MSN
Registration
STD
Engine
Operator
330-303
330-302
330-202
330-343
330-323
330-323
1514
1515
1516
1517
1518
1519
TC-JOB
EC-MAA
2406
9H-HFE
HL8293
B-5940
ST8
ST8
ST7
ST8
ST8
ST8
CF6-80E1A3
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
PW4168A
PW4170
CES06 0003
ETD13 0002
CPA11 0002
ETD12 0002
330-243
330-243
330-343
330-243F
1520
1521
1523
1524
B-5943
A6-EYU
B-LBE
D-ALMA
ST7
ST7
ST8
ST9
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CCA07 0008
USA02 0015
CEB01 0004
CSC02 0003
THY08 0007
HAL01 0018
PAL05 0002
CRK01 0011
XFA01 0013
ONE01 0002
AAW03 0002
CSN04 0006
330-343
330-243
330-343
330-343
330-303
330-243
330-343
330-343
330-343
330-243F
330-302
330-323
1525
1526
1527
1528
1529
1530
1531
1532
1533
1534
1535
1536
B-5946
N293AY
RP-C3344
B-5945
TC-JOD
N373HA
9H-SMF
B-5950
9M-XXS
N335QT
5A-ONR
B-5951
ST8
ST7
ST8
ST8
ST8
ST7
ST8
ST8
ST8
ST9
ST8
ST8
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
CF6-80E1A3
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
PW4170
CES06 0004
CCA07 0009
CAL04 0006
ONE02 0003
CCA07 0010
SKY01 0003
LAA01 0004
SIA05 0009
330-243
330-343
330-302
330-243
330-343
330-343
330-202
330-343
1537
1538
1539
1540
1541
1542
1543
1544
B-5949
B-5947
B-18361
EP-IJA
B-5948
TC-LOC
5A-LAU
2-SCCA
ST7
ST8
ST8
ST7
ST8
ST8
ST7
ST8
TRENT772C-60
TRENT772C-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CPA11 0003
PAL05 0003
CES06 0005
GIA03 0002
XFA01 0014
ONE01 0003
CES07 0001
CEB01 0005
PAL05 0004
SKY01 0004
78V01 0012
KAL06 0001
330-343
330-343
330-243
330-343
330-343
330-243F
330-343
330-343
330-343
330-343
330-243
330-323
1545
1546
1547
1548
1549
1550
1551
1552
1553
1554
1555
1556
B-LBF
RP-C8763
B-5952
PK-GPT
9M-XXT
TC-JOU
B-5953
RP-C3345
RP-C8764
TC-LOD
G-VYGL
HL8001
ST8
ST8
ST7
ST8
ST8
ST9
ST8
ST8
ST8
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
CPA11 0004
CHH01 0001
PAL05 0005
GIA03 0003
VOZ01 0006
330-343
330-243
330-343
330-343
330-243
1557
1558
1559
1560
1561
B-LBG
B-5955
RP-C8765
PK-GPU
VH-XFJ
ST8
ST7
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
SIA05 0010
CCA07 0011
ALK03 0001
330-343
330-343
330-343
1562
1563
1564
9V-SSD
B-5956
4R-ALL
ST8
ST8
ST8
TRENT772B-60
TRENT772C-60
TRENT772B-60
TURKISH AIRLINES CO.
IBERIA
ROYAL SAUDI AIR FORCE
SERAPH AVIATION
ASIANA AIRLINES, INC.
CHINA SOUTHERN
AIRLINES
CHINA EASTERN AIRLINES
ETIHAD AIRWAYS
CATHAY PACIFIC
EUROPEAN AIR
TRANSPORT
AIR CHINA LIMITED
AMERICAN AIRLINES, INC.
CEBU AIR, INC
SICHUAN AIRLINES
TURKISH AIRLINES CO.
HAWAIIAN AIRLINES, INC.
PHILIPPINE AIRLINES, INC.
HAINAN AIRLINES
AIRASIA X BERHAD
AVIANCA CARGO
AFRIQIYAH AIRWAYS
CHINA SOUTHERN
AIRLINES
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
CHINA AIRLINES LTD
IRAN AIR
AIR CHINA LIMITED
TURKISH AIRLINES CO.
LIBYAN AIRLINES
SGI- AVIATION SERVICES
B.V.
CATHAY PACIFIC
PHILIPPINE AIRLINES, INC.
CHINA EASTERN AIRLINES
GARUDA INDONESIA
AIRASIA X BERHAD
TURKISH AIRLINES CO.
CHINA EASTERN AIRLINES
CEBU AIR, INC
PHILIPPINE AIRLINES, INC.
TURKISH AIRLINES CO.
AIRTANKER SERVICES
KOREAN AIR LINES CO.
LTD
CATHAY PACIFIC
HAINAN AIRLINES
PHILIPPINE AIRLINES, INC.
GARUDA INDONESIA
COMMONWEALTH BANK
OF AUSTRALIA
SINGAPORE AIRLINES LTD
AIR CHINA LIMITED
SRILANKAN AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 24
MAINTENANCE PLANNING DOCUMENT
Version
Rank
HAL01 0019
PAL05 0006
CPA11 0005
PAL05 0007
CES06 0006
CCA07 0012
THY08 0008
OMA03 0001
CHH01 0002
SKY01 0005
CSN05 0001
Model
MSN
Registration
STD
Engine
Operator
330-243
330-343
330-343
330-343
330-243
330-343
330-303
330-343
330-243
330-343
330-323
1565
1566
1567
1568
1569
1570
1571
1572
1573
1574
1575
N374HA
RP-C8766
B-LBH
RP-C8771
B-5961
B-5957
TC-JOE
A4O-DH
B-5963
EC-MHL
B-5959
ST7
ST8
ST8
ST8
ST7
ST8
ST8
ST8
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772C-60
CF6-80E1A3
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
KAL06 0002
330-323
1576
HL8002
ST8
PW4170
GIA03 0004
QTR12 0001
CSC02 0004
KLM03 0005
330-343
330-243F
330-343
330-303
1577
1578
1579
1580
PK-GPV
HA-LHU
B-5960
PH-AKF
ST8
ST9
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
CF6-80E1A3
XFA01 0015
OMA03 0002
ALK03 0002
QTR12 0002
GIA03 0005
ONE02 0004
CCA07 0013
CES06 0007
XFA01 0016
KAL06 0003
330-343
330-343
330-343
330-243F
330-343
330-243
330-343
330-243
330-343
330-323
1581
1582
1583
1584
1585
1586
1587
1588
1589
1590
9M-XXU
A4O-DI
4R-ALM
OO-CGM
PK-GPW
EP-IJB
B-5958
B-5962
9M-XXV
HL8003
ST8
ST8
ST8
ST9
ST8
ST7
ST8
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772C-60
TRENT772B-60
PW4170
CHH01 0003
SKY01 0006
CSN05 0002
330-243
330-343
330-323
1591
1592
1593
B-5979
TC-LOE
B-5965
ST7
ST8
ST8
TRENT772B-60
TRENT772B-60
PW4170
QTR12 0003
CES07 0002
XFA01 0017
SIA05 0011
CPA11 0006
OMA03 0003
XFA01 0018
78V01 0013
CEB01 0006
CES06 0008
ALK03 0003
ARG01 0001
HAL01 0020
SKY01 0007
ONE02 0005
SIA05 0012
78V01 0014
KAL06 0004
330-243F
330-343
330-343
330-343
330-343
330-343
330-343
330-243
330-343
330-243
330-343
330-202
330-243
330-343
330-243
330-343
330-243
330-323
1594
1595
1596
1597
1598
1599
1600
1601
1602
1603
1604
1605
1606
1607
1608
1609
1610
1611
OO-SEA
B-5969
9M-XXW
9V-SSE
B-LBI
A4O-DJ
9M-XXY
G-VYGM
RP-C3346
B-5968
4R-ALN
LV-FVH
N375HA
TC-LOJ
F-UJCS
9V-SSF
G-VYGN
HL8025
ST9
ST8
ST8
ST8
ST8
ST8
ST8
ST7
ST8
ST7
ST8
ST7
ST7
ST8
ST7
ST8
ST7
ST8
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
XFA01 0019
DAH02 0001
CRK01 0012
330-343
330-202
330-343
1612
1613
1614
9M-XXZ
7T-VJA
B-5971
ST8
ST7
ST8
TRENT772B-60
CF6-80E1A4
TRENT772B-60
HAWAIIAN AIRLINES, INC.
PHILIPPINE AIRLINES, INC.
CATHAY PACIFIC
PHILIPPINE AIRLINES, INC.
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
TURKISH AIRLINES CO.
OMAN AIR
HAINAN AIRLINES
AIR EUROPA
CHINA SOUTHERN
AIRLINES
KOREAN AIR LINES CO.
LTD
GARUDA INDONESIA
WIZZ AIR HUNGARY LTD.
SICHUAN AIRLINES
KLM ROYAL DUTCH
AIRLINES
AIRASIA X BERHAD
OMAN AIR
SRILANKAN AIRLINES
AIR BELGIUM SA
GARUDA INDONESIA
IRAN AIR
AIR CHINA LIMITED
CHINA EASTERN AIRLINES
AIRASIA X BERHAD
KOREAN AIR LINES CO.
LTD
HAINAN AIRLINES
TURKISH AIRLINES CO.
CHINA SOUTHERN
AIRLINES
AIR BELGIUM SA
CHINA EASTERN AIRLINES
AIRASIA X BERHAD
AERCAP IRELAND LIMITED
CATHAY PACIFIC
OMAN AIR
SERAPH AVIATION
AIRTANKER SERVICES
CEBU AIR, INC
CHINA EASTERN AIRLINES
SRILANKAN AIRLINES
AEROLINEAS ARGENTINAS
HAWAIIAN AIRLINES, INC.
TURKISH AIRLINES CO.
DGA
SINGAPORE AIRLINES LTD
AIRTANKER SERVICES
KOREAN AIR LINES CO.
LTD
AIRASIA X BERHAD
AIR ALGERIE
HAINAN AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 25
MAINTENANCE PLANNING DOCUMENT
Version
Rank
HAL01 0021
THY09 0001
CES06 0009
CPA10 0011
XFA01 0020
THY09 0002
CPA11 0007
THY09 0003
ARG01 0002
SKY01 0008
CSN05 0003
Model
MSN
Registration
STD
Engine
Operator
330-243
330-303
330-243
330-343
330-343
330-303
330-343
330-303
330-202
330-343
330-323
1615
1616
1617
1618
1619
1620
1621
1622
1623
1624
1625
N378HA
TC-JOF
B-5973
B-LBJ
HS-XTE
TC-JOG
B-LBK
TC-JOH
LV-FVI
TC-LOK
B-5966
ST7
ST8
ST7
ST8
ST8
ST8
ST8
ST8
ST7
ST8
ST8
TRENT772B-60
CF6-80E1A3
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
CF6-80E1A4
TRENT772B-60
PW4170
KAC02 0001
330-243
1626
9K-APA
ST7
TRENT772B-60
DAL01 0001
DAL01 0003
THY09 0004
DAH02 0002
TAR01 0001
CES07 0003
SIA05 0013
CRK01 0013
SKY01 0009
CSN05 0004
330-302
330-302
330-303
330-202
330-243
330-343
330-343
330-343
330-343
330-323
1627
1628
1629
1630
1631
1632
1633
1634
1635
1636
N822NW
N823NW
TC-JOI
7T-VJB
TS-IFM
B-5976
9V-SSG
B-5972
TC-LOF
B-5967
ST8
ST8
ST8
ST7
ST7
ST8
ST8
ST8
ST8
ST8
CF6-80E1A4
CF6-80E1A4
CF6-80E1A3
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
DAL01 0002
KAL06 0005
330-302
330-323
1637
1638
N824NW
HL8026
ST8
ST8
CF6-80E1A4
PW4170
CES06 0010
THY09 0005
TAR01 0002
THY09 0006
KAC02 0002
330-243
330-303
330-243
330-303
330-243
1639
1640
1641
1642
1643
B-5975
TC-JOJ
TS-IFN
TC-JOK
9K-APB
ST7
ST8
ST7
ST8
ST7
TRENT772C-60
CF6-80E1A3
TRENT772B-60
CF6-80E1A3
TRENT772B-60
THY09 0007
CSN05 0005
330-303
330-323
1644
1645
TC-JOL
B-5970
ST8
ST8
CF6-80E1A3
PW4170
XFA01 0021
KAL06 0006
330-343
330-323
1646
1647
HS-XTF
HL8027
ST8
ST8
TRENT772B-60
PW4170
SIA05 0014
DAH02 0003
ALK03 0004
SKY01 0010
KAC02 0003
330-343
330-202
330-343
330-343
330-243
1648
1649
1650
1651
1653
9V-SSH
7T-VJC
4R-ALO
TC-LOG
9K-APC
ST8
ST7
ST8
ST8
ST7
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
GIA03 0006
CES06 0011
CRK01 0014
ONE02 0006
CCA07 0014
XFA01 0022
SAS03 0001
330-343
330-243
330-343
330-243
330-343
330-343
330-343
1654
1655
1656
1657
1658
1659
1660
PK-GPX
B-8226
B-8015
F-UJCT
B-5977
9M-XBC
LN-RKR
ST8
ST7
ST8
ST7
ST8
ST8
ST8
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
CSC01 0004
330-243
1662
B-8332
ST7
TRENT772C-60
HAWAIIAN AIRLINES, INC.
TURKISH AIRLINES CO.
CHINA EASTERN AIRLINES
CATHAY PACIFIC
AIRASIA X BERHAD
TURKISH AIRLINES CO.
CATHAY PACIFIC
TURKISH AIRLINES CO.
AEROLINEAS ARGENTINAS
TURKISH AIRLINES CO.
CHINA SOUTHERN
AIRLINES
KUWAIT AIRWAYS
COMPANY
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
TURKISH AIRLINES CO.
AIR ALGERIE
TUNISAIR
CHINA EASTERN AIRLINES
SINGAPORE AIRLINES LTD
HAINAN AIRLINES
TURKISH AIRLINES CO.
CHINA SOUTHERN
AIRLINES
DELTA AIR LINES, INC.
KOREAN AIR LINES CO.
LTD
CHINA EASTERN AIRLINES
TURKISH AIRLINES CO.
TUNISAIR
TURKISH AIRLINES CO.
KUWAIT AIRWAYS
COMPANY
TURKISH AIRLINES CO.
CHINA SOUTHERN
AIRLINES
AIRASIA X BERHAD
KOREAN AIR LINES CO.
LTD
SINGAPORE AIRLINES LTD
AIR ALGERIE
SRILANKAN AIRLINES
TURKISH AIRLINES CO.
KUWAIT AIRWAYS
COMPANY
GARUDA INDONESIA
CHINA EASTERN AIRLINES
HAINAN AIRLINES
DGA
AIR CHINA LIMITED
AIRASIA X BERHAD
SCANDINAVIAN AIRLINES
SYSTEM
SICHUAN AIRLINES
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 26
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CRK01 0015
Model
MSN
Registration
STD
Engine
Operator
330-343
1663
B-8016
ST8
TRENT772C-60
CES06 0012
SAS03 0002
330-243
330-343
1664
1665
B-8231
LN-RKS
ST7
ST8
TRENT772C-60
TRENT772B-60
SIA05 0015
SAF01 0001
330-343
330-243
1666
1667
9V-SSI
760
ST8
ST7
TRENT772B-60
TRENT772B-60
CRK01 0016
ALK03 0005
XFA01 0023
GIA03 0007
HAL01 0022
CCA07 0015
XFA01 0024
LNI01 0001
15T01 0001
330-343
330-343
330-343
330-343
330-243
330-343
330-343
330-343
330-243
1668
1669
1670
1671
1672
1673
1674
1675
1676
B-LNQ
4R-ALP
9M-XBA
PK-GPY
N379HA
B-5978
9M-XBB
PK-LEF
HZ-SKY2
ST8
ST8
ST8
ST8
ST7
ST8
ST8
ST8
ST7
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CRK01 0017
KAC02 0004
330-343
330-243
1677
1678
B-8117
9K-APD
ST8
ST7
TRENT772B-60
TRENT772B-60
DAL01 0004
LNI01 0002
KAC02 0005
330-302
330-343
330-243
1679
1680
1681
N825NW
PK-LEG
9K-APE
ST8
ST8
ST7
CF6-80E1A4
TRENT772B-60
TRENT772B-60
EVA04 0001
330-302
1684
B-16335
ST8
CF6-80E1A4
CCA07 0016
CRK01 0018
ALK03 0006
QTR12 0004
ALK03 0007
EVA04 0002
330-343
330-343
330-343
330-243F
330-343
330-302
1685
1686
1687
1688
1689
1690
B-6101
B-8118
4R-ALQ
OO-CMA
4R-ALR
B-16336
ST8
ST8
ST8
ST9
ST8
ST8
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
EVE01 0001
FJI02 0001
LNI01 0003
IBE09 0001
CCA07 0017
THY09 0008
SAS03 0003
330-343
330-343
330-343
330-202
330-343
330-303
330-343
1691
1692
1693
1694
1695
1696
1697
EC-MII
DQ-FJW
PK-LEH
EC-MIL
B-6102
TC-LNC
LN-RKT
ST8
ST8
ST8
ST7
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772C-60
CF6-80E1A3
TRENT772B-60
GIA04 0001
CSN05 0006
330-343
330-323
1698
1699
PK-GPZ
B-8358
ST8
ST8
TRENT772B-60
PW4170
IBE09 0002
DAL01 0005
CRK01 0019
THY09 0009
THY09 0010
QTR12 0005
GIA04 0002
IBE09 0003
EDW03 0001
CEB01 0007
THY09 0011
330-202
330-302
330-343
330-303
330-303
330-243F
330-343
330-202
330-343
330-343
330-303
1700
1701
1703
1704
1706
1708
1709
1710
1711
1712
1713
EC-MJA
N826NW
B-8287
TC-LND
TC-LNE
OO-AIR
PK-GHA
EC-MJT
D-AFYR
RP-C3347
TC-LNF
ST7
ST8
ST8
ST8
ST8
ST9
ST8
ST7
ST8
ST8
ST8
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
CF6-80E1A3
CF6-80E1A3
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CF6-80E1A3
LUCKY AIR COMPANY,
LIMITED
CHINA EASTERN AIRLINES
SCANDINAVIAN AIRLINES
SYSTEM
SINGAPORE AIRLINES LTD
REP OF SINGAPORE AIR
FORCE
HONG KONG AIRLINES LTD
SRILANKAN AIRLINES
AIRASIA X BERHAD
GARUDA INDONESIA
HAWAIIAN AIRLINES, INC.
AIR CHINA LIMITED
AIRASIA X BERHAD
LION MENTARI AIRLINES
SKY PRIME AVIATION
SERVICES
HAINAN AIRLINES
KUWAIT AIRWAYS
COMPANY
DELTA AIR LINES, INC.
LION MENTARI AIRLINES
KUWAIT AIRWAYS
COMPANY
EVA AIRWAYS
CORPORATION
AIR CHINA LIMITED
HAINAN AIRLINES
SRILANKAN AIRLINES
AIR BELGIUM SA
SRILANKAN AIRLINES
EVA AIRWAYS
CORPORATION
EVELOP AIRLINES S.L.
AIR PACIFIC LIMITED
LION MENTARI AIRLINES
IBERIA
AIR CHINA LIMITED
TURKISH AIRLINES CO.
SCANDINAVIAN AIRLINES
SYSTEM
GARUDA INDONESIA
CHINA SOUTHERN
AIRLINES
IBERIA
DELTA AIR LINES, INC.
HAINAN AIRLINES
TURKISH AIRLINES CO.
TURKISH AIRLINES CO.
AIR BELGIUM SA
GARUDA INDONESIA
IBERIA
EW DISCOVER GMBH
CEBU AIR, INC
TURKISH AIRLINES CO.
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 27
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CSN05 0007
Model
MSN
Registration
STD
Engine
Operator
330-323
1714
B-8359
ST8
PW4170
SAS03 0004
330-343
1715
LN-RKU
ST8
TRENT772B-60
DAL01 0006
THY09 0012
IBE09 0004
DAL01 0007
DAL01 0008
THY11 0001
GIA04 0003
SVA03 0001
MEA03 0001
SVA03 0002
FWI03 0001
IBE09 0005
SVA03 0003
TBA01 0001
SVA03 0004
HAL01 0023
GIA04 0004
SVA03 0005
FAF01 0001
330-302
330-303
330-202
330-302
330-302
330-243F
330-343
330-343
330-243
330-343
330-323
330-202
330-343
330-243
330-343
330-243
330-343
330-343
330-243
1716
1718
1719
1720
1721
1722
1723
1724
1725
1726
1727
1728
1729
1730
1731
1732
1733
1734
1735
N827NW
TC-LNG
EC-MKI
N828NW
N829NW
TC-JOV
PK-GHC
HZ-AQ11
OD-MEE
HZ-AQ12
F-HPUJ
EC-MKJ
HZ-AQ13
B-8420
HZ-AQ14
N360HA
PK-GHD
HZ-AQ15
F-UJCG
ST8
ST8
ST7
ST8
ST8
ST9
ST8
ST8
ST7
ST8
ST8
ST7
ST8
ST7
ST8
ST7
ST8
ST8
ST7
CF6-80E1A4
CF6-80E1A3
CF6-80E1A4
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
IBE09 0006
ARG01 0003
SVA03 0006
SVA03 0007
IBE09 0007
RWD01
0001
EIN04 0001
SVA03 0008
EIN04 0002
SAA04 0001
CSC03 0001
IBE09 0008
ARG01 0004
SVA03 0009
THY11 0002
08N01 0001
330-202
330-202
330-343
330-343
330-202
330-243
1736
1737
1738
1739
1740
1741
EC-MLB
LV-GHQ
HZ-AQ16
HZ-AQ17
EC-MLP
9XR-WN
ST7
ST7
ST8
ST8
ST7
ST7
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CHINA SOUTHERN
AIRLINES
SCANDINAVIAN AIRLINES
SYSTEM
DELTA AIR LINES, INC.
TURKISH AIRLINES CO.
IBERIA
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
TURKISH AIRLINES CO.
GARUDA INDONESIA
SAUDIA
MIDDLE EAST AIRLINES
SAUDIA
AIR CARAIBES
IBERIA
SAUDIA
TIBET AIRLINES CO. LTD
SAUDIA
HAWAIIAN AIRLINES, INC.
GARUDA INDONESIA
SAUDIA
FORCE AERIENNE
FRANCAISE
IBERIA
AEROLINEAS ARGENTINAS
SAUDIA
SAUDIA
IBERIA
RWANDAIR LTD.
330-302
330-343
330-302
330-343
330-243
330-202
330-202
330-343
330-243F
330-243
1742
1743
1744
1745
1746
1747
1748
1749
1750
1751
EI-FNG
HZ-AQ18
EI-FNH
ZS-SXI
B-8468
EC-MMG
LV-GIF
HZ-AQ19
TC-JOY
VP-BHD
ST8
ST8
ST8
ST8
ST7
ST7
ST7
ST8
ST9
ST7
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
CCA07 0018
CBJ01 0001
SAA04 0002
IBE09 0009
GCR01 0001
SAA04 0003
GCR01 0002
RWD02
0001
CSN05 0008
330-343
330-343
330-343
330-202
330-243
330-343
330-243
330-343
1752
1753
1754
1755
1756
1757
1758
1759
B-8577
B-8678
ZS-SXJ
EC-MNK
B-8776
ZS-SXK
B-8659
9XR-WP
ST8
ST8
ST8
ST7
ST7
ST8
ST7
ST8
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772B-60
TRENT772B-60
TRENT772B-60
330-323
1760
B-8426
ST8
PW4170
IBE09 0010
SAF01 0002
330-202
330-243
1761
1762
EC-MNL
761
ST7
ST7
CF6-80E1A4
TRENT772B-60
ISSUE: JUL 01/21
Effectivity Cross Reference Table
AER LINGUS LTD
SAUDIA
AER LINGUS LTD
CMB FINANCIAL LEASING
SICHUAN AIRLINES
IBERIA
AEROLINEAS ARGENTINAS
SAUDIA
TURKISH AIRLINES CO.
JET AVIATION BUSINESS
JETS (HK
AIR CHINA LIMITED
BEIJING CAPITAL AIRLINES
AIRBORNE CAPITAL LTD
IBERIA
TIANJIN AIRLINES CO. LTD
CMB FINANCIAL LEASING
TIANJIN AIRLINES CO. LTD
RWANDAIR LTD.
CHINA SOUTHERN
AIRLINES
IBERIA
REP OF SINGAPORE AIR
FORCE
Page 28
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CBJ01 0002
SVA03 0010
CCA07 0019
SVA03 0011
EVA04 0003
Model
MSN
Registration
STD
Engine
Operator
330-343
330-343
330-343
330-343
330-302
1763
1764
1765
1766
1767
B-8679
HZ-AQ20
B-8579
HZ-AQ21
B-16337
ST8
ST8
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
THY11 0003
DAL01 0009
SVA03 0012
TBA01 0002
ETD12 0003
330-243F
330-302
330-343
330-243
330-243F
1768
1769
1770
1771
1772
TC-JOZ
N830NW
HZ-AQ22
B-8950
D-ALEJ
ST9
ST8
ST8
ST7
ST9
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
GCR01 0003
SVA03 0013
GCR01 0004
CSN05 0009
330-243
330-343
330-243
330-323
1773
1774
1775
1776
B-8959
HZ-AQ23
B-8981
B-8870
ST7
ST8
ST7
ST8
TRENT772B-60
TRENT772B-60
TRENT772B-60
PW4170
IBE09 0011
EVA04 0004
330-202
330-302
1777
1778
EC-MOU
B-16338
ST7
ST8
CF6-80E1A4
CF6-80E1A4
SAA04 0004
CSC03 0002
SVA03 0014
GCR01 0005
DAL01 0010
IBE09 0012
TBA01 0003
CCA07 0020
12P01 0001
330-343
330-243
330-343
330-243
330-302
330-202
330-243
330-343
330-243
1779
1780
1781
1782
1783
1784
1785
1786
1787
9H-HFA
B-8962
HZ-AQ24
B-8982
N831NW
EC-MOY
B-8951
B-8689
18-001
ST8
ST7
ST8
ST7
ST8
ST7
ST7
ST8
ST7
TRENT772B-60
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
TRENT772C-60
TRENT772C-60
TRENT772B-60
CES08 0001
CEB01 0008
SVA03 0015
EIN05 0001
SAA04 0005
CSN05 0010
330-343
330-343
330-343
330-302
330-343
330-323
1788
1789
1790
1791
1792
1793
B-8968
RP-C3348
HZ-AQ25
EI-GAJ
ZS-SXM
B-8360
ST8
ST8
ST8
ST8
ST8
ST8
TRENT772C-60
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
PW4170
EVA04 0005
330-302
1794
B-16339
ST8
CF6-80E1A4
D0015 0001
CES08 0002
SVA03 0016
CES08 0003
SAF01 0003
330-941
330-343
330-343
330-343
330-243
1795
1796
1797
1798
1799
F-WTTN
B-8967
HZ-AQ26
B-8970
762
STH
ST8
ST8
ST8
ST7
TRENT7000-72
TRENT772C-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
SVA03 0017
CES08 0004
CCA07 0021
SVA03 0018
CES08 0005
GCR01 0006
EVA04 0006
330-343
330-343
330-343
330-343
330-343
330-243
330-302
1800
1801
1802
1803
1804
1805
1806
HZ-AQ27
B-8971
B-8383
HZ-AQ28
B-8972
B-8596
B-16340
ST8
ST8
ST8
ST8
ST8
ST7
ST8
TRENT772B-60
TRENT772C-60
TRENT772C-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
CCA07 0022
FAF01 0002
330-343
330-243
1807
1808
B-8385
F-UJCH
ST8
ST7
TRENT772C-60
TRENT772B-60
BEIJING CAPITAL AIRLINES
SAUDIA
AIR CHINA LIMITED
SAUDIA
EVA AIRWAYS
CORPORATION
TURKISH AIRLINES CO.
DELTA AIR LINES, INC.
SAUDIA
TIBET AIRLINES CO. LTD
EUROPEAN AIR
TRANSPORT
TIANJIN AIRLINES CO. LTD
SAUDIA
BEIJING CAPITAL AIRLINES
CHINA SOUTHERN
AIRLINES
IBERIA
EVA AIRWAYS
CORPORATION
HI FLY MALTA
SICHUAN AIRLINES
SAUDIA
BEIJING CAPITAL AIRLINES
DELTA AIR LINES, INC.
IBERIA
TIBET AIRLINES CO. LTD
AIR CHINA LIMITED
REPUBLIC OF KOREA AIR
FORCE
CHINA EASTERN AIRLINES
CEBU AIR, INC
SAUDIA
AER LINGUS LTD
SOUTH AFRICAN AIRWAYS
CHINA SOUTHERN
AIRLINES
EVA AIRWAYS
CORPORATION
AIRBUS
CHINA EASTERN AIRLINES
SAUDIA
CHINA EASTERN AIRLINES
REP OF SINGAPORE AIR
FORCE
SAUDIA
CHINA EASTERN AIRLINES
AIR CHINA LIMITED
SAUDIA
CHINA EASTERN AIRLINES
TIANJIN AIRLINES CO. LTD
EVA AIRWAYS
CORPORATION
AIR CHINA LIMITED
FORCE AERIENNE
FRANCAISE
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 29
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CES08 0006
CSZ01 0001
Model
MSN
Registration
STD
Engine
Operator
330-343
330-343
1809
1810
B-8862
B-8865
ST8
ST8
TRENT772C-60
TRENT772C-60
CCA07 0023
SVA03 0019
D0016 0001
CSN06 0001
330-343
330-343
330-941
330-343
1811
1812
1813
1814
B-8386
HZ-AQ29
F-WTTE
B-8361
ST8
ST8
STH
ST8
TRENT772C-60
TRENT772B-60
TRENT7000-72
TRENT772C-60
CSN06 0002
330-343
1815
B-8362
ST8
TRENT772C-60
CES08 0007
EIN05 0002
CSN06 0003
330-343
330-302
330-343
1816
1817
1818
B-8863
EI-GCF
B-8363
ST8
ST8
ST8
TRENT772C-60
CF6-80E1A4
TRENT772C-60
TAP03 0001
MXD01 0001
CSN06 0004
330-941
330-343
330-343
1819
1820
1821
CS-TUA
PK-LEL
B-8365
STH
ST8
ST8
TRENT7000-72
TRENT772B-60
TRENT772C-60
SAF01 0004
330-243
1822
763
ST7
TRENT772B-60
HAL01 0024
AIB10 0001
CSC04 0001
CSN06 0005
330-243
330-743L
330-343
330-343
1823
1824
1825
1826
N361HA
F-GXLG
B-8690
B-8366
ST7
STL
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772C-60
CHH02 0001
MXD01 0002
CSZ01 0002
330-343
330-343
330-343
1827
1828
1829
B-1022
PK-LEK
B-1017
ST8
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
01Q01 0001
330-243
1830
T-054
ST7
TRENT772B-60
CHH02 0002
MXD01 0003
CES08 0008
SVA03 0020
IBE09 0013
TAP03 0002
CHH02 0003
CHH02 0004
330-343
330-343
330-343
330-343
330-202
330-941
330-343
330-343
1831
1832
1833
1834
1835
1836
1837
1838
B-1021
PK-LEM
B-1049
HZ-AQ30
EC-MSY
CS-TUB
B-1020
B-1059
ST8
ST8
ST8
ST8
ST7
STH
ST8
ST8
TRENT772B-60
TRENT772B-60
TRENT772C-60
TRENT772B-60
CF6-80E1A4
TRENT7000-72
TRENT772B-60
TRENT772B-60
CSZ01 0003
330-343
1839
B-1036
ST8
TRENT772C-60
CHH02 0005
CES08 0009
CES08 0010
CHH02 0006
330-343
330-343
330-343
330-343
1840
1841
1842
1843
B-1045
B-1066
B-1041
B-1004
ST8
ST8
ST8
ST8
TRENT772B-60
TRENT772C-60
TRENT772C-60
TRENT772B-60
BER01 0001
TBA01 0004
CSN06 0006
330-941
330-243
330-343
1844
1845
1846
OO-ABF
B-1047
B-1062
STH
ST7
ST8
TRENT7000-72
TRENT772C-60
TRENT772C-60
CBJ02 0001
12P01 0002
330-243
330-243
1847
1848
B-1043
19-002
ST7
ST7
TRENT772B-60
TRENT772B-60
CHH02 0007
TAP03 0003
330-343
330-941
1849
1850
B-302D
CS-TUC
ST8
STH
TRENT772B-60
TRENT7000-72
CHINA EASTERN AIRLINES
SHENZHEN AIRLINES CO.,
LTD.
AIR CHINA LIMITED
SAUDIA
AIRBUS
CHINA SOUTHERN
AIRLINES
CHINA SOUTHERN
AIRLINES
CHINA EASTERN AIRLINES
AER LINGUS LTD
CHINA SOUTHERN
AIRLINES
TAP AIR PORTUGAL
PT. BATIK AIR INDONESIA
CHINA SOUTHERN
AIRLINES
REP OF SINGAPORE AIR
FORCE
HAWAIIAN AIRLINES, INC.
ATI
SICHUAN AIRLINES
CHINA SOUTHERN
AIRLINES
HAINAN AIRLINES
PT. BATIK AIR INDONESIA
SHENZHEN AIRLINES CO.,
LTD.
NATO SUPPORT AND
PROCUREMENT A
HAINAN AIRLINES
PT. BATIK AIR INDONESIA
CHINA EASTERN AIRLINES
SAUDIA
IBERIA
TAP AIR PORTUGAL
HAINAN AIRLINES
LUCKY AIR COMPANY,
LIMITED
SHENZHEN AIRLINES CO.,
LTD.
TIANJIN AIRLINES CO. LTD
CHINA EASTERN AIRLINES
CHINA EASTERN AIRLINES
LUCKY AIR COMPANY,
LIMITED
AIR BELGIUM SA
TIBET AIRLINES CO. LTD
CHINA SOUTHERN
AIRLINES
BEIJING CAPITAL AIRLINES
REPUBLIC OF KOREA AIR
FORCE
TIANJIN AIRLINES CO. LTD
TAP AIR PORTUGAL
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 30
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CHH02 0008
Model
MSN
Registration
STD
Engine
Operator
330-343
1851
B-1014
ST8
TRENT772C-60
CSN06 0007
330-343
1852
B-1063
ST8
TRENT772C-60
AIB10 0002
IBE09 0014
CHH02 0009
CSC04 0002
SAF01 0005
330-743L
330-202
330-343
330-343
330-243
1853
1854
1855
1856
1857
F-GXLH
EC-MUD
B-1048
B-8589
764
STL
ST7
ST8
ST8
ST7
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
TRENT772B-60
CSN06 0008
330-343
1858
B-1065
ST8
TRENT772C-60
TBA01 0005
CHH02 0010
BER01 0002
CHH02 0011
CRK03 0001
IBE09 0015
CRK03 0002
CHH02 0012
330-243
330-343
330-941
330-343
330-343
330-202
330-343
330-343
1859
1860
1861
1862
1863
1864
1865
1866
B-1046
B-1097
OO-ABG
B-1042
B-LHF
F-HLVL
B-LHG
B-305W
ST7
ST8
STH
ST8
ST8
ST7
ST8
ST8
TRENT772C-60
TRENT772B-60
TRENT7000-72
TRENT772B-60
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT772C-60
CSZ01 0004
330-343
1867
B-1072
ST8
TRENT772C-60
CES08 0011
CES08 0012
WOW01
0001
CHH02 0013
HFY01 0001
330-343
330-343
330-941
1868
1869
1870
B-300Q
B-1073
PK-GYA
ST8
ST8
STH
TRENT772C-60
TRENT772C-60
TRENT7000-72
LUCKY AIR COMPANY,
LIMITED
CHINA SOUTHERN
AIRLINES
ATI
IBERIA
HAINAN AIRLINES
SICHUAN AIRLINES
REP OF SINGAPORE AIR
FORCE
CHINA SOUTHERN
AIRLINES
TIBET AIRLINES CO. LTD
HAINAN AIRLINES
AIR BELGIUM SA
BEIJING CAPITAL AIRLINES
AIRBUS
OPENSKIES
AIRBUS
LUCKY AIR COMPANY,
LIMITED
SHENZHEN AIRLINES CO.,
LTD.
CHINA EASTERN AIRLINES
CHINA EASTERN AIRLINES
PT CITILINK INDONESIA
330-343
330-243
1871
1872
B-1096
9N-ALY
ST8
ST7
TRENT772B-60
TRENT772B-60
CES08 0013
CRK03 0003
CHH02 0014
AZU01 0001
IBE09 0016
HFY01 0002
330-343
330-343
330-343
330-941
330-202
330-243
1873
1874
1875
1876
1877
1878
B-300P
B-LHH
B-1098
PR-ANZ
EC-MYA
9N-ALZ
ST8
ST8
ST8
STH
ST7
ST7
TRENT772C-60
TRENT772B-60
TRENT772B-60
TRENT7000-72
CF6-80E1A4
TRENT772B-60
CSZ01 0005
330-343
1879
B-302E
ST8
TRENT772C-60
CHH02 0015
CES08 0014
IBE09 0017
12P01 0003
330-343
330-343
330-202
330-243
1880
1881
1882
1883
B-305R
B-303D
F-HLVM
19-003
ST8
ST8
ST7
ST7
TRENT772B-60
TRENT772C-60
CF6-80E1A4
TRENT772B-60
MAU04 0001
CSN06 0009
330-941
330-343
1884
1885
3B-NBU
B-300V
STH
ST8
TRENT7000-72
TRENT772C-60
SAF01 0006
330-243
1886
765
ST7
TRENT772B-60
WOW01
0002
D0017 0001
CSZ01 0006
330-941
1887
PK-GYC
STH
TRENT7000-72
330-841
330-343
1888
1889
F-WTTO
B-303N
STG
ST8
TRENT7000-72
TRENT772C-60
MAU04 0002
12P01 0004
330-941
330-243
1890
1891
3B-NBV
19-004
STH
ST7
TRENT7000-72
TRENT772B-60
ISSUE: JUL 01/21
Effectivity Cross Reference Table
HAINAN AIRLINES
NEPAL AIRLINES
CORPORATION
CHINA EASTERN AIRLINES
AIRBUS
HAINAN AIRLINES
AZUL
IBERIA
NEPAL AIRLINES
CORPORATION
SHENZHEN AIRLINES CO.,
LTD.
BEIJING CAPITAL AIRLINES
CHINA EASTERN AIRLINES
OPENSKIES
REPUBLIC OF KOREA AIR
FORCE
AIR MAURITIUS
CHINA SOUTHERN
AIRLINES
REP OF SINGAPORE AIR
FORCE
PT CITILINK INDONESIA
AIRBUS
SHENZHEN AIRLINES CO.,
LTD.
AIR MAURITIUS
REPUBLIC OF KOREA AIR
FORCE
Page 31
MAINTENANCE PLANNING DOCUMENT
Version
Rank
TAP03 0004
CHH02 0016
CSN06 0010
Model
MSN
Registration
STD
Engine
Operator
330-941
330-343
330-343
1892
1893
1894
CS-TUD
B-304L
B-300U
STH
ST8
ST8
TRENT7000-72
TRENT772B-60
TRENT772C-60
AZU01 0002
CHH02 0017
TAP03 0005
CHH02 0018
CHH02 0019
TAP03 0006
WOW01
0003
CRK03 0004
WOW01
0004
TAP03 0007
CES08 0015
TAP03 0008
CRK03 0005
TAP03 0009
TAP03 0010
SZN01 0001
01Q01 0002
330-941
330-343
330-941
330-343
330-343
330-941
330-941
1895
1896
1897
1898
1899
1900
1901
PR-ANY
B-303C
CS-TUE
B-303Z
B-304K
CS-TUF
HS-XJA
STH
ST8
STH
ST8
ST8
STH
STH
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT772B-60
TRENT772B-60
TRENT7000-72
TRENT7000-72
TAP AIR PORTUGAL
HAINAN AIRLINES
CHINA SOUTHERN
AIRLINES
AZUL
HAINAN AIRLINES
TAP AIR PORTUGAL
HAINAN AIRLINES
HAINAN AIRLINES
TAP AIR PORTUGAL
AIRASIA X BERHAD
330-343
330-941
1902
1903
B-LHI
HS-XJB
ST8
STH
TRENT772B-60
TRENT7000-72
AIRBUS
AIRASIA X BERHAD
330-941
330-343
330-941
330-343
330-941
330-941
330-941
330-243
1904
1905
1906
1907
1908
1909
1910
1911
CS-TUG
B-304A
CS-TUH
B-LHJ
CS-TUI
CS-TUJ
9H-SZN
T-055
STH
ST8
STH
ST8
STH
STH
STH
ST7
TRENT7000-72
TRENT772C-60
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
CSC04 0003
TAP03 0011
TAP03 0012
DAL02 0001
FAF01 0003
330-343
330-941
330-941
330-941
330-243
1912
1913
1914
1915
1916
B-308F
CS-TUK
CS-TUL
N401DZ
F-UJCI
ST8
STH
STH
STH
ST7
TRENT772C-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
CHH02 0020
TAP03 0013
01Q01 0003
330-343
330-941
330-243
1917
1918
1919
B-005C
CS-TUM
T-056
ST8
STH
ST7
TRENT772B-60
TRENT7000-72
TRENT772B-60
DAL02 0002
TAP03 0014
TAP03 0015
SZN01 0002
AZU01 0003
TAP03 0016
LNI02 0001
LNI02 0002
SAS03 0005
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-343
1920
1921
1922
1923
1924
1925
1926
1927
1928
N402DX
CS-TUN
CS-TUO
6V-ANB
PR-ANX
CS-TUP
PK-LEI
PK-LEJ
SE-REH
STH
STH
STH
STH
STH
STH
STH
STH
ST8
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
HFY02 0001
AIB10 0003
DAL02 0003
IBE09 0018
LNI02 0003
AZU01 0004
DAL02 0004
IBE09 0019
ACI02 0001
330-941
330-743L
330-941
330-202
330-941
330-941
330-941
330-202
330-941
1929
1930
1931
1932
1933
1934
1935
1936
1937
CS-TKY
F-GXLI
N403DX
EC-NEN
PK-LES
PR-ANW
N404DX
EC-NNH
F-ONEO
STH
STL
STH
ST7
STH
STH
STH
ST7
STH
TRENT7000-72
TRENT772B-60
TRENT7000-72
CF6-80E1A4
TRENT7000-72
TRENT7000-72
TRENT7000-72
CF6-80E1A4
TRENT7000-72
ACI02 0002
330-941
1938
F-ONET
STH
TRENT7000-72
TAP AIR PORTUGAL
CHINA EASTERN AIRLINES
TAP AIR PORTUGAL
AIRBUS
TAP AIR PORTUGAL
TAP AIR PORTUGAL
HI FLY MALTA
NATO SUPPORT AND
PROCUREMENT A
SICHUAN AIRLINES
TAP AIR PORTUGAL
TAP AIR PORTUGAL
DELTA AIR LINES, INC.
FORCE AERIENNE
FRANCAISE
BEIJING CAPITAL AIRLINES
TAP AIR PORTUGAL
NATO SUPPORT AND
PROCUREMENT A
DELTA AIR LINES, INC.
TAP AIR PORTUGAL
TAP AIR PORTUGAL
AIR SENEGAL S.A.
AZUL
TAP AIR PORTUGAL
LION MENTARI AIRLINES
LION MENTARI AIRLINES
SCANDINAVIAN AIRLINES
SYSTEM
HI FLY
ATI
DELTA AIR LINES, INC.
IBERIA
LION MENTARI AIRLINES
AZUL
DELTA AIR LINES, INC.
IBERIA
AIR CALEDONIE
INTERNATIONAL
AIR CALEDONIE
INTERNATIONAL
ISSUE: JUL 01/21
Effectivity Cross Reference Table
Page 32
MAINTENANCE PLANNING DOCUMENT
Version
Rank
LNI02 0004
TAP03 0017
FAF01 0004
Model
MSN
Registration
STD
Engine
Operator
330-941
330-941
330-243
1939
1941
1942
PK-LET
CS-TUQ
F-UJCJ
STH
STH
ST7
TRENT7000-72
TRENT7000-72
TRENT772B-60
TAP03 0018
01Q01 0004
330-941
330-243
1943
1945
CS-TUR
T-057
STH
ST7
TRENT7000-72
TRENT772B-60
GIA05 0003
GIA05 0001
GIA05 0002
DAL02 0005
EIN05 0003
EIN05 0004
AZU01 0005
DAL02 0006
TAP03 0019
LNI02 0005
DAL02 0007
GIA05 0004
GIA05 0005
01Q01 0005
330-941
330-941
330-941
330-941
330-302
330-302
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-243
1946
1947
1948
1949
1950
1951
1952
1953
1954
1956
1957
1958
1959
1960
PK-GHG
PK-GHE
PK-GHF
N405DX
EI-EIM
EI-EIN
PR-ANV
N406DX
CS-TUS
PK-LEQ
N407DX
PK-GHH
PK-GHI
T-058
STH
STH
STH
STH
ST8
ST8
STH
STH
STH
STH
STH
STH
STH
ST7
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
CF6-80E1A4
CF6-80E1A4
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
GIA05 0006
DAL02 0008
EVE02 0001
KAC03 0001
330-941
330-941
330-941
330-841
1961
1962
1963
1964
PK-GHJ
N408DX
CS-TKH
9K-APF
STH
STH
STH
STG
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
FAF01 0005
330-243
1965
F-UJCK
ST7
TRENT772B-60
CFG01 0001
330-941
1966
STH
TRENT7000-72
CEB02 0007
FAF01 0006
330-941
330-243
1967
1968
EC-333
STH
ST7
TRENT7000-72
TRENT772B-60
KAC03 0002
330-841
1969
9K-APG
STG
TRENT7000-72
CEB02 0004
XAX05 0003
XAX05 0005
CEB02 0005
CRL04 0001
CEB02 0006
UGD01 0001
LNI02 0006
UGD01 0002
XLF02 0001
01Q01 0006
DAL02 0009
LNI02 0007
AIB10 0004
CRL04 0002
LNI02 0008
GIA05 0007
01Q01 0007
DAL02 0010
DAL02 0011
330-941
330-941
330-941
330-941
330-941
330-941
330-841
330-941
330-841
330-941
330-243
330-941
330-941
330-743L
330-941
330-941
330-941
330-243
330-941
330-941
1970
1971
1972
1973
1975
1976
1977
1978
1979
1981
1982
1983
1984
1985
1986
1987
1988
1989
1990
1991
STH
STH
STH
STH
STH
STH
STG
STH
STG
STH
ST7
STH
STH
STL
STH
STH
STH
ST7
STH
STH
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT7000-72
LION MENTARI AIRLINES
TAP AIR PORTUGAL
FORCE AERIENNE
FRANCAISE
TAP AIR PORTUGAL
NATO SUPPORT AND
PROCUREMENT A
GARUDA INDONESIA
GARUDA INDONESIA
GARUDA INDONESIA
DELTA AIR LINES, INC.
AER LINGUS LTD
AER LINGUS LTD
AZUL
DELTA AIR LINES, INC.
TAP AIR PORTUGAL
LION MENTARI AIRLINES
DELTA AIR LINES, INC.
GARUDA INDONESIA
GARUDA INDONESIA
NATO SUPPORT AND
PROCUREMENT A
GARUDA INDONESIA
DELTA AIR LINES, INC.
ORBEST S.A.
KUWAIT AIRWAYS
COMPANY
FORCE AERIENNE
FRANCAISE
CONDOR FLUGDIENST
GMBH
CEBU AIR, INC
FORCE AERIENNE
FRANCAISE
KUWAIT AIRWAYS
COMPANY
CEBU AIR, INC
AIRBUS
AIRBUS
CEBU AIR, INC
CORSAIR S.A.
CEBU AIR, INC
UGANDA AIRLINES
LION MENTARI AIRLINES
UGANDA AIRLINES
XL AIRWAYS FRANCE
OCCAR
DELTA AIR LINES, INC.
LION MENTARI AIRLINES
ATI
CORSAIR S.A.
LION MENTARI AIRLINES
GARUDA INDONESIA
OCCAR
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
ISSUE: JUL 01/21
F-HRNB
5X-NIL
PK-LER
5X-CRN
EC-338
N409DX
PK-LEU
F-GXLJ
F-HSKA
PK-LEV
EC-340
N410DZ
N411DX
Effectivity Cross Reference Table
Page 33
MAINTENANCE PLANNING DOCUMENT
Version
Rank
CRL04 0003
CRL04 0004
DAL02 0012
DAL02 0015
DAL02 0013
DAL02 0014
FAF01 0007
Model
MSN
Registration
STD
Engine
Operator
330-941
330-941
330-941
330-941
330-941
330-941
330-243
1992
1993
1994
1995
1996
1997
1998
F-WWCU
F-WWKD
STH
STH
STH
STH
STH
STH
ST7
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
DAL02 0017
DAL02 0016
CEB02 0001
CEB02 0002
SJX01 0001
330-941
330-941
330-941
330-941
330-941
1999
2000
2001
2002
2003
STH
STH
STH
STH
STH
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
CEB02 0003
KAC03 0003
330-941
330-841
2004
2005
STH
STG
TRENT7000-72
TRENT7000-72
SJX01 0002
330-941
2006
STH
TRENT7000-72
FAF01 0010
330-243
2007
ST7
TRENT772B-60
FAF01 0008
330-243
2008
EC-336
ST7
TRENT772B-60
CRL04 0005
DAL02 0018
FAF01 0009
330-941
330-941
330-243
2009
2010
2011
EC-337
STH
STH
ST7
TRENT7000-72
TRENT7000-72
TRENT772B-60
FAF01 0011
330-243
2012
ST7
TRENT772B-60
SJX01 0003
330-941
2013
STH
TRENT7000-72
DAL02 0019
FAF01 0012
330-941
330-243
2014
2015
STH
ST7
TRENT7000-72
TRENT772B-60
KAC03 0004
330-841
2016
STG
TRENT7000-72
SJX01 0004
330-941
2017
STH
TRENT7000-72
VIR10 0001
GRL01 0001
FAF01 0013
330-941
330-841
330-243
2018
2020
2022
STH
STG
ST7
TRENT7000-72
TRENT7000-72
TRENT772B-60
UAF02 0001
330-243
2023
ST7
TRENT772B-60
AIB10 0005
MEA04 0001
AIB10 0006
AIB07 0001
AIB06 0001
AIB05 0001
AIB05 0002
AIB08 0001
AIB09 0001
AIB11 0001
AIB14 0001
AIB15 0001
330-743L
330-941
330-743L
330-321
330-343
330-202F
330-203F
330-841
330-941
330-941
330-941
330-941
2027
2032
2041
4122
4123
4202
4203
4841
4941
4942
4943
4944
STL
STH
STL
ST8
ST8
ST9
ST9
STG
STH
STH
STH
STH
TRENT772B-60
TRENT7000-72
TRENT772B-60
PW4164
TRENT772B-60
CF6-80E1A4
CF6-80E1A3
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
CORSAIR S.A.
CORSAIR S.A.
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
FORCE AERIENNE
FRANCAISE
DELTA AIR LINES, INC.
DELTA AIR LINES, INC.
CEBU AIR, INC
CEBU AIR, INC
STARLUX AIRLINES CO.,
LTD.
CEBU AIR, INC
KUWAIT AIRWAYS
COMPANY
STARLUX AIRLINES CO.,
LTD.
FORCE AERIENNE
FRANCAISE
FORCE AERIENNE
FRANCAISE
CORSAIR S.A.
DELTA AIR LINES, INC.
FORCE AERIENNE
FRANCAISE
FORCE AERIENNE
FRANCAISE
STARLUX AIRLINES CO.,
LTD.
DELTA AIR LINES, INC.
FORCE AERIENNE
FRANCAISE
KUWAIT AIRWAYS
COMPANY
STARLUX AIRLINES CO.,
LTD.
VIRGIN ATLANTIC
AIR GREENLAND
FORCE AERIENNE
FRANCAISE
UNITED ARAB EMIRATES
AIR FORCE
ATI
MIDDLE EAST AIRLINES
ATI
ISSUE: JUL 01/21
N413DX
N414DZ
N415DX
EC-339
F-WWKP
9K-APH
Effectivity Cross Reference Table
Page 34
MAINTENANCE PLANNING DOCUMENT
Version
Rank
AIB16 0001
AIB17 0001
AIB19 0001
AIB26 0001
AIB26 0002
AIB26 0003
AIB18 0001
AIB21 0001
AIB33 0001
AIB27 0001
AIB28 0001
AIB28 0002
AIB27 0002
AIB28 0003
AIB28 0004
AIB27 0003
AIB28 0005
AIB27 0004
AIB28 0006
AIB27 0005
LNI03 0001
IRA02 0001
AIB29 0001
AIB29 0002
AIB29 0003
AIB29 0004
AIB29 0005
AIB29 0006
AIB29 0007
C9G05 0001
AIB25 0001
AIB31 0001
AIB38 0001
AIB10 0007
XAX05 0001
AIB24 0001
XAX05 0002
XAX05 0007
XAX05 0008
XAX05 0006
XAX05 0004
Model
MSN
330-941
330-941
330-243
330-941
330-941
330-941
330-941
330-743L
330-202
330-243
330-202
330-202
330-243
330-202
330-202
330-243
330-202
330-243
330-202
330-243
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-941
330-243
330-743L
330-941
330-941
330-941
330-941
330-941
330-941
330-941
4945
4946
5007
5013
5014
5015
5019
5021
5409
5412
5413
5414
5417
5418
5421
5423
5427
5429
5430
5431
5433
5449
5450
5451
5452
5453
5454
5455
5456
5457
5458
5459
5780
5824
5966
5967
5970
5971
5972
5973
5976
ISSUE: JUL 01/21
Registration
STD
Engine
STH
STH
ST7
STH
STH
STH
STH
STL
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
ST7
STH
STH
STH
STH
STH
STH
STH
STH
STH
STH
STH
STH
ST7
STL
STH
STH
STH
STH
STH
STH
STH
TRENT7000-72
TRENT7000-72
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
CF6-80E1A4
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT772B-60
TRENT772B-60
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
TRENT7000-72
Effectivity Cross Reference Table
Operator
IRAN AIR
AIRBUS
AIRBUS
AIRASIA X BERHAD
AIRASIA X BERHAD
AIRASIA X BERHAD
Page 35
MAINTENANCE PLANNING DOCUMENT
SERVICE BULLETIN LIST
The following table lists the MOD SBs, which are stated in the Applicability column of the MPD Task Data.
SB
Number
00-3033
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
00-3068
IN PROGRESS
21-3028
IN PROGRESS
21-3046
IN PROGRESS
21-3049
IN PROGRESS
21-3060
IN PROGRESS
21-3061
IN PROGRESS
21-3066
IN PROGRESS
21-3074
IN PROGRESS
21-3076
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
GENERAL - NON STANDARD
ITEMS LIST - INSTALLATION
OF VARIOUS SYSTEMS
MODIFICATIONS ON A330
MSN 455 FOR COMMONALITY
WITH UAE CONFIGURATION
GENERAL- A330/340 FAMILY
LIFE TIME EXTENSIONCERTIFY INTERMEDIATE
SERVICE GOAL STEP 2
AIR CONDITIONING-AVIONIC
EQUIPT. VENTIL.ADD WATER
DRAINAGE ON AVIONICS
VENTIL. CIRCUIT & IMPROVE
WATER DRAINAGE OF GRU
AIR CONDITIONING COCKPIT AND CABIN
TEMPERATURE CONTROL INSTALL A SIX-AREA
TEMPERATURE CONTROL
SYSTEM.
AIR CONDITIONING COCKPIT AND CABIN
TEMPERATURE CONTROL RELOCATE THE CABIN
TEMPERATURE SENSORS
AIR CONDITIONING INTRODUCE TWO OZONE
CATALYTIC CONVERTERS AIR CONDITIONING AVIONICS EQUIPMENT
VENTILATION - IMPROVE
AVIONICS VENTILATION
SYSTEM AND GROUND
REFRIGERATION SYSTEM TO
PREVENT WATER INGRESS
IN RACKS.
AIR CONDITIONING - PACK
CONTROL AND INDICATING INTRODUCE PACK
CONTROLLER -06
LOWER DECK CARGO
COMPARTMENT
VENTILATION AND COOLING
- RE-INSTALL LOWER DECK
FORWARD CARGO
COMPARTMENT
VENTILATION AND
TEMPERATURE CONTROL
AIR CONDITIONING GENERAL - MODIFY PACK
OUTLET DUCT AND CLAMP
Service Bulletin
Page 1
MAINTENANCE PLANNING DOCUMENT
SB
Number
21-3093
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
21-3094
IN PROGRESS
21-3095
IN PROGRESS
21-3096
IN PROGRESS
21-3111
IN PROGRESS
21-3115
IN PROGRESS
21-3128
IN PROGRESS
21-3149
IN PROGRESS
21-3153
IN PROGRESS
21-3155
IN PROGRESS
21-3174
IN PROGRESS
23-3124
IN PROGRESS
23-3251
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
AIR CONDITIONING AVIONICS EQUIPMENT
GROUND COOLING REMOVE THE GROUND
REFRIGERATION UNIT (GRU).
AIR CONDITIONING AVIONICS EQUIPMENT
GROUND COOLING - DEACTIVATE THE GROUND
REFRIGERATION UNIT (GRU).
AIR CONDITIONING AVIONICS EQUIPMENT
GROUND COOLING - MODIFY
AIR COOLING SYSTEM
AIR CONDITIONING - CENTER
FUSELAGE - INSTALL
HEATSHIELDS IN BELLY
FAIRING TO SEGREGATE AIR
SYSTEM.
AIR CONDITIONING - PACK
CONTROL AND INDICATING INTRODUCE NEW PACK
CONTROLLER STANDARD
AIR CONDITIONING - AIR
CONDITIONING (PACKS) INTRODUCE IMPROVED
SEALS
AIR CONDITIONING COMPARTMENT
VENTILATION - MODIFY
ISOLATION VALVE MPD TASK
AND PIN PROGRAMMING
FOR LDMCR CONTAINER W/O
STAIRHOUSE
AIR CONDITIONING -OZONE
CONVERTER - INSTALL
OZONE CATALYTIC
CONVERTERS
AIR CONDITIONING - BULK
CARGO COMPARTMENT INSTALL CARGO HEATING
AIR CONDITIONING - CABIN
AIR DISTRIBUTION AND
RECIRCULATION - REMOVE
ICEGRIDS FROM THE MAIN
DECK AIR SUPPLY DUCTS.
AIR CONDITIONING CONDITIONED SERVICE AIR
SYSTEM (CSAS) INTRODUCE NEW OZONE
CONVERTER AT CSAS.
COMMUNICATIONS EMERGENCY ALERTING
SYSTEM INSTALLATION
COMMUNICATIONS SATELLITE TV/DATA
TRANSCEIVER SYSTEM REMOVE CONNEXION BY
BOEING (CBB) SYSTEM
Service Bulletin
Page 2
MAINTENANCE PLANNING DOCUMENT
SB
Number
24-3008
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
24-3045
IN PROGRESS
24-3049
IN PROGRESS
24-3050
IN PROGRESS
25-3110
IN PROGRESS
25-3114
IN PROGRESS
25-3161
IN PROGRESS
25-3168
IN PROGRESS
25-3194
IN PROGRESS
25-3249
IN PROGRESS
25-3324
IN PROGRESS
25-3336
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
ELECTRICAL POWER REPLACE A330 IDG AND
INSTALL WIRING ON IDGGCUS.
ELECTRICAL POWER - APU
GENERATOR - INTRODUCE A
SECONDARY HOUSING TO
THE APU GENERATOR.
ELECTRICAL POWER GENERAL - IMPROVE
SHEDDING OF COMMERCIAL
DC LOADS
ELECTRICAL POWER GENERAL - IMPROVE
SHEDDING OF COMMERCIAL
DC LOADS
EQUIPMENT/FURNISHINGS IMPROVE ATTACHMENT
SYSTEM OF CAPT AND F/O
FOOTRESTS AND
ASSOCIATED DAMPERS.
EQUIPMENT/FURNISHINGS CARGO COMPARTMENTS INTRODUCE NEW PDU
CONTROL BOX
EQUIPMENT/FURNISHING PASSENGER COMPARTMENT
- INTRODUCE A MODIFIED
INTRUSION AND
PENETRATION RESISTANT
COCKPIT DOOR
EQUIPMENT/FURNISHINGS CREW REST ROOM
(UNDERFLOOR) - INSTALL
THE PROVISIONS FOR AN
UNDERFLOOR CREW REST
CONTAINER
EQUIPMENT/FURNISHINGS COCKPIT -INSTALL
PENETRATION RESISTANT
COCKPIT DOOR STEP 2 ON
AIRCRAFT FITTED WITH
COCKPIT DOOR STEP 1
FUSELAGE - COCKPIT
INSTRUMENT PANEL
INSTALLATION - REPLACE
BRACKET.
EQUIPMENT/FURNISHING FWD AND AFT CARGO
COMPARTMENT - INSTALL
HEATED DRAINAGE
EQUIPMENT / FURNISHINGS LAVATORIES - INSTALL A
FILTER IN POTABLE WATER
SUPPLY IN EACH LAVATORY
Service Bulletin
Page 3
MAINTENANCE PLANNING DOCUMENT
SB
Number
25-3363
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
25-3436
IN PROGRESS
25-3493
IN PROGRESS
25-3520
IN PROGRESS
25-3548
IN PROGRESS
25-3583
IN PROGRESS
25-3588
IN PROGRESS
25-3591
IN PROGRESS
25-3593
IN PROGRESS
25-3595
IN PROGRESS
25-3596
IN PROGRESS
25-3598
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
EQUIPMENT/FURNISHINGS CREW REST ROOM (CABIN) INSTALL THE PROVISIONS
FOR AN UNDERFLOOR CREW
REST CONTAINER
EQUIPMENT/FURNISHING FWD AND AFT CARGO
COMPARTMENT - INSTALL
HEATED DRAINAGE
EQUIPMENT/FURNISHINGCURTAINS AND PARTITIONS INTRODUCE IMPROVED
DECOMPRESSION PANEL IN
COCKPIT DOOR
EQUIPMENT/FURNISHING FWD AND AFT CARGO
COMPARTMENT - INSTALL
HEATED DRAINAGE ON
AIRCRAFT WITH ADVANCED
CLS
EQUIPMENT/FURNISHINGS COCKPIT - REINFORCE
INSTRUMENT PANEL
BRACKET 6 (SB ONLY).
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
Service Bulletin
Page 4
MAINTENANCE PLANNING DOCUMENT
SB
Number
25-3600
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
25-3601
IN PROGRESS
25-3602
IN PROGRESS
25-3603
IN PROGRESS
25-3605
IN PROGRESS
25-3607
IN PROGRESS
25-3609
IN PROGRESS
25-3611
IN PROGRESS
25-3612
IN PROGRESS
25-3625
IN PROGRESS
25-3643
IN PROGRESS
25-3676
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
EQUIPMENT / FURNISHINGS LAVATORIES - SUPPLY
GASEOUS OXYGEN BOXES
FOR REPLACEMENT IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT/FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN BOXES IN
LAVATORIES
EQUIPMENT / FURNISHINGS COCKPIT - INSTALL A
REINFORCED COCKPIT
DOOR
EQUIPMENT/FURNISHINGS FWD AND AFT CARGO
COMPARTMENT - INSTALL
HEATED DRAINAGE
MISCELLANEOUS
EMERGENCY EQUIPMENT INSTALL LOW FREQUENCY
UNDERWATER LOCATOR
BEACON (LF-ULB)
Service Bulletin
Page 5
MAINTENANCE PLANNING DOCUMENT
SB
Number
25-3691
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
25-3699
IN PROGRESS
25-3704
IN PROGRESS
25-3718
IN PROGRESS
25-3728
IN PROGRESS
26-3020
IN PROGRESS
27-3023
IN PROGRESS
27-3039
IN PROGRESS
27-3040
IN PROGRESS
27-3054
IN PROGRESS
27-3069
IN PROGRESS
27-3075
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN CONTAINERS IN
LAVATORIES (15 MIN)
FWD AND AFT CARGO
COMPARTMENT - INSTALL
HEATED DRAINAGE ON
AIRCRAFT WITH ADVANCED
CLS
EQUIPMENT / FURNISHINGS LAVATORIES - REPLACE
CHEMICAL BY GASEOUS
OXYGEN CONTAINERS IN
LAVATORIES (22 MIN)
MISCELLANEOUS
EMERGENCY EQUIPMENT INSTALL LOW FREQUENCY
UNDERWATER LOCATOR
BEACON (LF-ULB)
MISCELLANEOUS
EMERGENCY EQUIPMENT INSTALL LOW FREQUENCY
UNDERWATER LOCATOR
BEACON (LF-ULB)
FIRE PROTECTION DETECTION - MODIFY
SMOKE DETECTION
CONTROL UNIT (SDCU)
FLIGHT CONTROLS - FLAPS INSTALL KAMATICS FLAP
TRACK ROLLER BEARINGS.
FLIGHT CONTROLS - EFCS /
CONTROL INPUT AND
POWER SUPPLY - PROVIDE A
SECOND ELECTRICAL
POWER SUPPLY TO FCSC2.
FLIGHT CONTROLS - EFCS
CONTROL INPUS AND
POWER SUPPLY - PROVIDE A
SECOND ELECTRICAL
POWER SUPPLY TO FCPC3.
FLIGHT CONTROLS AILERON - INTRODUCE
SERVO CONTROLS TO ECP-9
STD.
FLIGHT CONTROLS RUDDER TRAVEL LIMITATION
UNIT - INSTALL NEW
STANDARD EQUIPMENT, PN
343500M00.
FLIGHT CONTROLS AILERON AND SERVOCONTROL - AILERON
SERVOCONTROL ECP8
Service Bulletin
Page 6
MAINTENANCE PLANNING DOCUMENT
SB
Number
27-3076
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
27-3092
IN PROGRESS
27-3100
IN PROGRESS
27-3105
IN PROGRESS
27-3125
IN PROGRESS
27-3128
IN PROGRESS
27-3135
IN PROGRESS
27-3136
IN PROGRESS
27-3142
IN PROGRESS
27-3159
IN PROGRESS
27-3173
IN PROGRESS
27-3234
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FLIGHT CONTROLS ELEVATOR AND HYDRAULIC
ACTUATION - INTRODUCE
ROD EYE END ROLLER
BEARING ON ELEVATOR
SERVO-CONTROL
FLIGHT CONTROLS - WINGS OUTBOARD FLAP - INSTALL
MODIFIED SENSOR STRUT
AT TRACK 4
FLIGHT CONTROLS - SLATS INTRODUCE ROTARY
ACTUATOR WITH IMPROVED
TORQUE LIMITER ASSEMBLY
FLIGHT CONTROLS - SLATS INTRODUCE ROTARY
ACTUATOR WITH IMPROVED
TORQUE LIMITER
PERFORMANCE PN
954C0000-01
FLIGHT CONTROL - YAW
DAMPER ACTUATION INSTALL YAW DAMPER
SERVO ACTUATORS WITH
IMPROVED PISTON ROD
SEALING.
FLIGHT CONTROLS ELEVATOR AND HYDRAULIC
ACTUATION - INSTALL NEW
SERVOCONTROL FITTED
WITH AN IMPROVED MVT.
FLIGHT CONTROLSELEVATOR AND HYDRAULICREINTRODUCE INITIAL MODE
SELECTOR VALVE.
FLIGHT CONTROLS ELEVATOR AND HYDRAULIC
ACTUATION-INSTALL NEW
ELEVATOR SERVOCONTROL.
FLIGHT CONTROLS ELECTRICAL BACKUP INTRODUCE NEW BCM TO
RECOVER NOMINAL
BEHAVIOUR.
FLIGHT CONTROLS CONTROL INPUTS AND
POWER SUPPLY - PROVIDE A
SECOND ELECTRICAL
POWER SUPPLY TO FCPC3.
FLIGHT CONTROLS - FLAPS INTRODUCE NEW GREASING
PROCEDURE FOR DOWN
DRIVE SHAFTS TRACK 1-5.
TRIMMABLE HORIZONTAL
STABILIZER (THS)
HYDRAULIC ACTUATION INSTALL ELSD ON THSA
Service Bulletin
Page 7
MAINTENANCE PLANNING DOCUMENT
SB
Number
28-3014
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
28-3018
IN PROGRESS
28-3040
IN PROGRESS
28-3041
IN PROGRESS
28-3056
IN PROGRESS
28-3084
IN PROGRESS
28-3088
IN PROGRESS
28-3089
IN PROGRESS
28-3094
IN PROGRESS
28-3113
IN PROGRESS
29-3104
IN PROGRESS
31-3056
IN PROGRESS
31-3057
IN PROGRESS
31-3109
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FUEL - APU FUEL PUMP
SYSTEM - INTRODUCE
SHORTENED SUCTION LINE
IN AIR SEPARATOR.
FUEL - REFUEL/DEFUEL
SYSTEM - REFUEL
COUPLINGS ADDED TO L/H
WING.
FUEL - APU FUEL PUMP
SYSTEM - INTRODUCE NEW
APU AFT PUMP
FUEL - APU PUMP SYSTEM PREVENT ELECTRICAL
OVERLOAD FOR ESSENTIEL
NETWORK
FUEL - TRIM TANK
TRANSFER SYSTEM MODIFY CIRCUIT DESIGN TO
IMPROVE RELIABILITY - FUEL - JETTISON SYSTEM INSTALL JETTISON SYSTEM
ON A330-200
FUEL - TANK VENTING (RH) INTRODUCE NEW 2 INCH
FLOAT VENT VALVE AT
5208QS FOR BASIC LR
FUEL - TANK VENTING (LH) INTRODUCE NEW 0.5 INCH
FLOAT VENT VALVE IN TRIM
TANK AT POSITION 5216QS
FUEL - TANK VENTING
SYSTEM - REPLACE PN L8713-001 BY AN IMPROVED 0.5
INCH FLOAT VENT VALVE PN
L87-13-003
FUEL-MAIN TRANSFER SYSTINTRO GROUND FAULT
INTERRUPTERS TO CENTER
TANK FUEL PUMP CONTROL
CIRCUIT
HYDRAULIC POWER GENERAL - INTRODUCE
MODIFIED GROUND SERVICE
MANIFOLD
INDICATING/RECORDING
SYSTEMS - EIS - INSTALL
NEW THALES DISPLAY
SYSTEM (EIS2)
INDICATING/RECORDING
SYSTEMS - EIS - INSTALL
NEW EIS2 STANDARD L4-1
CAPABLE OF ALL LONG
RANGE AIRCRAFT.
A330 INDICATING/RECORDING INSTALL WIRELESS GROUND
LINK DAR
Service Bulletin
Page 8
MAINTENANCE PLANNING DOCUMENT
SB
Number
31-3119
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
31-3130
IN PROGRESS
31-3142
IN PROGRESS
31-3167
IN PROGRESS
31-3181
IN PROGRESS
31-3184
IN PROGRESS
31-3185
IN PROGRESS
31-3193
IN PROGRESS
31-3215
IN PROGRESS
31-3233
IN PROGRESS
31-3234
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
INDICATING/RECORDING
SYSTEMS - ACMS INSTALLATION OF WDAR (PN
2243800-73).
INDICATING/RECORDING
SYSTEMS - DFDRS - INSTALL
TELEDYNE WQAR 8 GSM
INDICATING / RECORDING
SYSTEMS - ACMS INSTALLATION OF A
TELEDYNE WGL-DAR 4GSM
WITH 1024MB PCMCIA
CARDS
INDICATING/RECORDING
SYSTEMS - ACMS INSTALLATION OF A
TELEDYNE WGL-DAR 8GSM
WITH 1024MB PCMCIA
CARDS
INDICATING/RECORDING
SYSTEMS - DFDRS - INSTALL
TELEDYNE WGL-QAR GSM
WITH 512MB PCMCIA
MEMORY CARDS
INDICATING/RECORDING
SYSTEMS - INSTALL A WGLDAR WITH 4 GSM MODULES
AND 512MB PCMCIA
MEMORY CARDS
INDICATING/RECORDING
SYSTEMS - DFDRS - INSTALL
TELEDYNE WQAR 4 GSM
WITH 1024MB PCMCIA
MEMORY CARDS
INDICATING / RECORDING
SYSTEMS - ACMS INSTALLATION OF A
TELEDYNE WGL-DAR 4GSM
WITH 1024MB PCMCIA
CARDS
INSTALLATION OF WGL-DAR
4 HSPA+ (ARINC 591/600)
TELEDYNE P/N 2243800-364
INDICATING/RECORDING
SYSTEMS - INSTALLATION
OF WGL-DAR NG 4-HSPA
(ARINC 591/600) TELEDYNE
WITH SOFTWARE P/N
2234507-2
INDICATING/RECORDING
SYSTEMS - INSTALL FULL
PROVISIONS FOR WGL-DAR
ARINC 591/600 FOR A/C WITH
WGL-QAR
Service Bulletin
Page 9
MAINTENANCE PLANNING DOCUMENT
SB
Number
31-3242
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
31-3253
IN PROGRESS
32-3030
IN PROGRESS
32-3072
IN PROGRESS
32-3083
IN PROGRESS
32-3086
IN PROGRESS
32-3135
IN PROGRESS
32-3164
IN PROGRESS
32-3180
IN PROGRESS
32-3192
IN PROGRESS
32-3227
IN PROGRESS
32-3234
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
DMC ACQUISITION /
INTERFACE - INSTALL
WIRING AND ACTIVATE
REVERSIBLE BACK-UP
SPEED SCALE (BUSS)
THROUGH PUSH BUTTON
FOR BUSS FUNCTION
INDICATING/RECORDING
SYSTEMS - EIS - INSTALL
ENHANCED EIS2 WITH L10
SOFTWARE
LANDING GEAR - NLG INSTALL A WARNING
SYSTEM FOR TOWING
ANGLE LIMIT.
LANDING GEAR - MLG - FIT
MODIFIED BEARING
HOUSING WITH KARON 'M'
COATING.
LANDING GEAR EMERGENCY BRAKING INSTALL A SHUT-OFF VALVE
LANDING GEAR - ALTERNATE
BRAKING - INSTALL THE
BRAKE DUAL
DISTRIBUTIONVALVE WITH
MODIFIED COVER.
LANDING GEAR - MAIN GEAR
- INTRODUCE NEW
ADJUSTABLE LINK WITH
SPLIT BALL INTEGRAL
BEARINGS
LANDING GEAR - NOSE
LANDING GEAR - INTRODUCE
A SEAL WITHIN THE
ROTATING STEERING
COLLAR TO PREVENT
GREASE MIGRATING INTO
RVDT GEARBOXES
LANDING GEAR - MAIN GEAR
- INTRODUCE NEW REDESIGNED PISTON ROD ON
THE RETRACTION
ACTUATOR
LANDING GEAR - NOSE GEAR
- INTRODUCE NEW
STEERING COLLAR AND
BUSHES TO IMPROVE
GREASING
LANDING GEAR - MAIN GEAR
- INTRODUCTION OF NEW
SM8 AND SM9 PIN
ASSEMBLIES
LANDING GEAR - NOSE GEAR
- DEACTIVATE OVER-STEER
WARNING SYSTEM ON INSERVICE AIRCRAFT
Service Bulletin
Page 10
MAINTENANCE PLANNING DOCUMENT
SB
Number
32-3235
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
32-3237
IN PROGRESS
32-3246
IN PROGRESS
32-3268
IN PROGRESS
33-3004
IN PROGRESS
34-3065
IN PROGRESS
34-3087
IN PROGRESS
34-3092
IN PROGRESS
34-3117
IN PROGRESS
34-3120
IN PROGRESS
34-3141
IN PROGRESS
34-3154
IN PROGRESS
34-3213
IN PROGRESS
34-3228
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
LANDING GEAR - NOSE GEAR
- REFURBISHMENT OF
EXISTING COLLAR AS AN
ALTERNATIVE SOLUTION TO
MOD 53073
LANDING GEAR - MAIN GEAR
- IMPROVED 2-PART PAINT
SCHEME FOR BASIC,
GROWTH AND ENHANCED
MLG BOGIE BEAM
LANDING GEAR - NOSE GEAR
- REINSTALL NLG
OVERSTEER WARNING
SYSTEM
LANDING GEAR - MAIN GEAR
- INTRODUCE NICKEL UNDER
CHROME PATCH AND NEW
BOGIESTOP PAD ON
ENHANCED MLG BOGIE
BEAM
LIGHTS - EMERGENCY
LIGHTING SYSTEM - INSTALL
MODIFIED EPSU.
NAVIGATION - WEATHER
RADAR SYSTEM - ACTIVATE
DUAL PREDICTIVE
WINDSHEAR RADAR
SYSTEM, COLLINS
NAVIGATION - ANGLE OF
ATTACK INDICATION INSTALL ANGLE OF ATTACK
SENSORS ROSEMOUNT.
NAVIGATION - WEATHER
RADAR SYSTEM - ACTIVATE
HONEYWELL PREDICTIVE
WINDSHEAR FUNCTION.
NAVIGATION - ATC - INSTALL
REMOTE ATC CONTROL BOX
NAVIGATION - STANDBY
NAVIGATION SYSTEMS INSTALL THALES AVIONICS
INTEGRATED STANDBY
INSTRUMENT SYSTEM (ISIS)
NAVIGATION - STANDBY
NAVIGATION SYSTEM INSTALL NEW ISIS
STANDARD PN C16221WA01
NAVIGATION - ATC/MODES DEACTIVATE RATC
FUNCTION.
NAVIGATION - ADIRS INTRODUCE BACK-UP SPEED
SCALE FUNCTION.
NAVIGATION - SENSORS
POWER SUPPLY AND
SWITCHING - INSTALL
THALES ANGLE OF ATTACK
SENSORS PN C16291AB
Service Bulletin
Page 11
MAINTENANCE PLANNING DOCUMENT
SB
Number
34-3230
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
34-3236
IN PROGRESS
34-3243
IN PROGRESS
34-3252
IN PROGRESS
34-3267
IN PROGRESS
34-3271
IN PROGRESS
34-3284
IN PROGRESS
34-3286
IN PROGRESS
34-3301
IN PROGRESS
34-3311
IN PROGRESS
34-3312
IN PROGRESS
34-3313
IN PROGRESS
34-3320
IN PROGRESS
34-3324
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
NAVIGATION - STANDBY
NAVIGATION SYSTEMS INSTALL THALES
INTEGRATED STANDBY
INSTRUMENT SYSTEM (ISIS)
WEATHER RADAR SYSTEM ACTIVATE OF PREDICTIVE
WINDSHEAR
NAVIGATION - ATC/MODE S DEACTIVATE RATC
FUNCTION
NAVIGATION - SWITCHING
AND INDICATING - REMOVE
DDRMI INDICATORS
NAVIGATION - STANDBY
NAVIGATION SYSTEMS INSTALL THALES
INTEGRATED STANDBY
INSTRUMENT SYSTEM V2
(ISIS)
NAVIGATION - T/TISS INSTALL T3CAS, BASED ON
T2CAS INSTALLATION
NAVIGATION - WEATHER
RADAR SYSTEM ACTIVATION OF ROCKWELL
COLLINS PREDICTIVE
WINDSHEAR FUNCTION
NAVIGATION - TRAFFIC AND
TERRAIN INTEGRATED
SURVEILLANCE (T/TISS) INSTALL ACSS T3CAS STD
1.2
NAVIGATION - T3CAS INSTALL T3CAS STANDARD
1.2
NAVIGATION - AIR DATA INSTALL AOA UTAS WITH
NEW O-RING DESIGN
NAVIGATION - WEATHER
RADAR SYSTEM INSTALLATION OF
ROCKWELL COLLINS
WEATHER RADAR WITH PWS
AND MULTISCAN FUNCTIONS
NAVIGATION - INSTALLATION
OF A DUAL ADF HONEYWELL P/N 066-500141202
NAVIGATION - TRAFFIC AND
TERRAIN INTEGRATED
SURVEILLANCE SYSTEM
(T/TISS) - INSTALL ACSS
T3CAS CORRECTIVE STD 1.3
NAVIGATION - T3CAS UPGRADE T3CAS TO
STANDARD 2
Service Bulletin
Page 12
MAINTENANCE PLANNING DOCUMENT
SB
Number
34-3376
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
35-3042
IN PROGRESS
36-3022
IN PROGRESS
36-3023
IN PROGRESS
36-3027
IN PROGRESS
36-3034
IN PROGRESS
38-3029
IN PROGRESS
38-3038
IN PROGRESS
46-3059
IN PROGRESS
46-3102
IN PROGRESS
46-3120
IN PROGRESS
47-3001
IN PROGRESS
47-3002
IN PROGRESS
47-3005
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
NAVIGATION - T3CAS INSTALL T3CAS ACSS STD
2.2 P/N 9005000-11206 FROM
TCAS CHANGE 7.1
OXYGEN - PASSENGER
OXYGEN - INSTALL
ADDITIONAL CHECK VALVES
ON EACH OF BASIC OXYGEN
CYLINDER FOR GASEOUS
SYSTEM
PNEUMATIC - DISTRIBUTION
- INTRODUCE NEW FLEXIBLE
CONNECTORS
PNEUMATIC - DISTRIBUTION
- INTRODUCE FLEXIBLE
CONNECTORS
PNEUMATIC - DISTRIBUTION
- INTRODUCE IMPROVED
BLEED AIR AND WING ANTIICING DUCT SEALS
PNEUMATIC - DISTRIBUTION
- INTRODUCE PTFE SEALS
ABS5800 INTO HOT AIR
SYSTEMS
WATER / WASTE - POTABLE
WATER SYSTEM INTRODUCE INDEPENDANT
PRESSURIZATION
WATER/WASTE - WASTE
WATER DRAIN - REPLACE
THE WASTE WATER DRAIN IN
THE LAVATORY WASHBASIN
INFORMATION SYSTEMS MAINTENANCE ACCESS
TERMINAL SYSTEM CONNECT OIT (ON BOARD
INFORMATION TERMINAL)
ON A/C BATTERY
ON-BOARD INFORMATION
TERMINAL - UNINSTALL EFB
CLASS III FOR OIT
INFORMATION SYSTEMS ON-BOARD INFO TERMINAL
(OIT) - DEACTIVATE OIT
WHEN TOTALLY
INOPERATIVE
INERT GAS SYSTEM PROVISION FOR FUEL TANK
INERTING SYSTEM (FTIS)
FOR A330
INERT GAS SYSTEM INSTALLATION OF FUEL
TANK INERTING SYSTEM
(FTIS)
INERT GAS SYSTEM SYSTEM PROVISIONS AND
FTIS INSTALLATION
Service Bulletin
Page 13
MAINTENANCE PLANNING DOCUMENT
SB
Number
47-3008
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
49-3028
IN PROGRESS
52-3044
IN PROGRESS
52-3046
IN PROGRESS
52-3067
IN PROGRESS
52-3068
IN PROGRESS
52-3086
IN PROGRESS
52-3105
IN PROGRESS
52-3106
IN PROGRESS
52-3108
IN PROGRESS
52-3110
IN PROGRESS
52-3111
IN PROGRESS
52-3112
IN PROGRESS
52-3113
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
INSTALLATION OF FUEL
TANK INERTING SYSTEM
(FTIS)
AIRBORNE AUXILIARY
POWER - STORAGE AND
DISTRIBUTION - INTRODUCE
AN ENHANCED
RECOGNITION OF OIL
SYSTEM CONTAMINATION
DOORS - AFT CARGO
COMPARTMENT DOOR REINFORCE THE
STRUCTURE
LANDING GEAR - NOSE GEAR
DOORS - REAR DOOR REINFORCE NR 5 HINGE.
DOORS - COCKPIT DOOR
RELEASE SYSTEM - INSTALL
ELECTRICAL OVERRIDE
SYSTEM UNDER MMEL
DOORS - FWD CARGO
COMPARTMENT DOOR REINFORCE DOOR
STRUCTURE
DOORS-SERVICE DOORSMODIFICATION OF LATCHING
MECHANISM OF POTABLE
WATER SERVICE PANEL
DOORS - FWD CARGO
COMPARTMENT DOOR REINFORCE FWD CARGO
DOOR STRUCTURE DUE TO
CRACKED FRAMES
DOORS - AFT CARGO
COMPARTMENT DOOR REINFORCE AFT CARGO
DOOR STRUCTURE
DOORS - SERVICE DOORS IMPROVE SERVICE PANEL
ACCESS DOORS IN SECTION
16 AND 18
FWD CARGO COMPARTMENT
DOOR - REINFORCE FWD
CARGO DOOR STRUCTURE
DUE TO CRACKED FRAMES
FWD CARGO COMPARTMENT
DOOR - REINFORCE FWD
CARGO DOOR STRUCTURE
DUE TO CRACKED FRAMES
DOORS - AFT CARGO
COMPARTMENT DOOR REINFORCE CARGO DOOR
STRUCTURE DUE TO
CRACKED FRAMES
DOORS - AFT CARGO
COMPARTMENT DOOR REINFORCE AFT CARGO
DOOR STRUCTURE DUE TO
CRACKED FRAME
Service Bulletin
Page 14
MAINTENANCE PLANNING DOCUMENT
SB
Number
52-3114
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
53-3013
IN PROGRESS
53-3015
IN PROGRESS
53-3016
IN PROGRESS
53-3019
IN PROGRESS
53-3021
IN PROGRESS
53-3023
IN PROGRESS
53-3038
IN PROGRESS
53-3039
IN PROGRESS
53-3049
IN PROGRESS
53-3050
IN PROGRESS
53-3059
IN PROGRESS
53-3060
IN PROGRESS
53-3062
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
DOORS - AFT CARGO
COMPARTMENT DOOR REINFORCE AFT CARGO
DOOR STRUCTURE DUE TO
CRACKED FRAME
FUSELAGE - CENTRE
FUSELAGE - REINFORCE
MEMBRANE LIAISON AT
FR47/48.
FUSELAGE - GENERAL REINFORCE JOINT AT FRAME
53.2
FUSELAGE - CONE/REAR
FUSELAGE - INTRODUCE
ACCESS DOOR TO AIR
SEPARATOR.
FUSELAGE - CENTER
FUSELAGE - REINFORCE
CLG DOOR/STRUCTURE
JOINT AREA.
FUSELAGE - GENERAL REINFORCE STRINGER 39
BETWEEN FR53.2/53.3.
FUSELAGE - CENTER
FUSELAGE - REINFORCE THE
DOORFRAMES FOR TYENCY
EXIT DOORS
FUSELAGE - BELLY FAIRING REINFORCE FR37.4
SUBSTRUCTURE.
FUSELAGE - CENTRE
FUSELAGE - REINFORCE
FRAMES 53.3 AND 53.5, LH
AND RH FOR THE TYPE A
EMERGENCY EXIT DOORS.
FUSELAGE - GENERAL BELLY FAIRINGS - MODIFY
THE ATTACHMENTS OF
STIFFENER 29 AND OF THE
LOWER WEB AT FR53.8.
FUSELAGE - FAIRING REINFORCE LOWER WEB
AND DOOR WEB JUNCTION
AT FR47 AND AT FR53.2.
FUSELAGE - REAR
FUSELAGE - REINFORCE
FRAME 65 AT STGR 27 RH
FUSELAGE - FWD AND REAR
FUSELAGE - REINFORCE
CARGO DOOR ACTUATOR
SUPPORT-BEAM
FUSELAGE - CENTER
FUSELAGE - REINFORCE
FRAME LOWER SECTIONS AT
THE STRINGER PASSAGE
AREAS.
Service Bulletin
Page 15
MAINTENANCE PLANNING DOCUMENT
SB
Number
53-3065
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
53-3071
IN PROGRESS
53-3076
IN PROGRESS
53-3086
IN PROGRESS
53-3093
IN PROGRESS
53-3109
IN PROGRESS
53-3112
IN PROGRESS
53-3114
IN PROGRESS
53-3115
IN PROGRESS
53-3126
IN PROGRESS
53-3127
IN PROGRESS
53-3128
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FUSELAGE - PASSENGER
DOOR 2 LH AND RH REINFORCE FRAME 33
BETWEEN STGR 13 AND 15
FUSELAGE - REAR
FUSELAGE - REINFORCE
LOWER TORSION BOX BEAM
FRAME 73A - 75A FUSELAGE - REAR
FUSELAGE - REINFORCE
FRAME 73A AT THE ANCHOR
NUT HOLES BELOW STGR17,
LH AND RH
FUSELAGE - FWD FUSELAGE
- REINFORCE THE
PASSENGER/CREW DOOR 2
CUTOUT CORNER AREAS
FUSELAGE - CENTER
FUSELAGE - REINFORCE
FRAME 40.
FUSELAGE - REAR
FUSELAGE - REINFORCE
FLOOR BEAM ATTACHMENTFITTINGS AT FRAMES 73A
AND 75A, STGR26, LH/RH
FUSELAGE - REAR
FUSELAGE - RELOCATE VHF
2 ANTENNA
FUSELAGE - REAR
FUSELAGE - REINFORCE
FR60 THRU FR64 AT THE
RUN-OUT OF FRAME
COUPLINGS, BETWEEN
STGR18 AND STGR22A (RH),
AND REINFORCE FR66 AT
COUPLING ADJACENT TO
STGR22X (RH)
FUSELAGE - NOSE
FORWARD FUSELAGE INSTALL NEW GENERATION
OF RADOME USING QUARTZ
MATERIAL.
FUSELAGE - CENTER
FUSELAGE - SPLICING
FRAME 40.3 TO 45, STGR 26
TO 29 - FATIGUE LIFE
IMPROVEMENT.
FUSELAGE - CENTER
FUSELAGE CIRCUMFERENTIAL JOINT
FRAME 53.3, STGR 13 LH TO
STGR 13 RH - FATIGUE LIFE
IMPROVEMENT
FUSELAGE - FORWARD
FUSELAGE CIRCUMFERENTIAL JOINT
FRAME 13 STR 9 - FATIGUE
LIFE IMPROVEMENT
Service Bulletin
Page 16
MAINTENANCE PLANNING DOCUMENT
SB
Number
53-3130
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
53-3136
IN PROGRESS
53-3143
IN PROGRESS
53-3144
IN PROGRESS
53-3145
IN PROGRESS
53-3164
IN PROGRESS
53-3166
IN PROGRESS
53-3169
IN PROGRESS
53-3222
IN PROGRESS
53-3223
IN PROGRESS
53-3224
IN PROGRESS
53-3225
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FUSELAGE - FORWARD
FUSELAGE - REINFORCE
FRAME 12A AREA.
FUSELAGE - CENTER
FUSELAGE - FRAME 40
FORWARD FITTING FLANGE
STR 39/40 FATIGUE LIFE
IMPROVEMENT.
FUSELAGE - CENTER
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT FR
53.3,STR 13 LH TO STR 13 RH
- FATIGUE LIFE
IMPROVEMENT.
FUSELAGE - CENTER
FUSELAGE CIRCUMFERENTIAL JOINTS
AT FRAME 45 AND 54
FATIGUE LIFE
IMPROVEMENT.
FUSELAGE - CENTER
FUSELAGE - FR 40
CIRCUMFERENTIAL STRAP
FATIGUE LIFE
IMPROVEMENT
FUSELAGE - GENERAL MODIFY PARTIALLY ORBITAL
JUNCTION IN SECTION 12,
FRAME 13.
FUSELAGE - BELLY FAIRING
FRAME WORK - USE OF
TITANIUM PROFILE.
FUSELAGE - CENTER
FUSELAGE - REINFORCE
ORBITAL LINK FRAME 45 TO
IMPROVE FATIGUE
BEHAVIOUR.
FUSELAGE - CENTER
FUSELAGE - IMPROVE
SPLICING AREA FROM
FRAME 48 TO 53-2 BETWEEN
STR.23 AND 26 LH/RH
FUSELAGE - FORWARD
FUSELAGE - REINFORCE
COUPLINGS IN AREA FR20 FR25 / STGR20 RH - STGR23
RH
FUSELAGE - REAR
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT AT
FR72
FUSELAGE - REAR
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT AT
FR58
Service Bulletin
Page 17
MAINTENANCE PLANNING DOCUMENT
SB
Number
53-3226
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
53-3236
IN PROGRESS
53-3237
IN PROGRESS
53-3238
IN PROGRESS
53-3244
IN PROGRESS
53-3248
IN PROGRESS
53-3250
IN PROGRESS
53-3251
IN PROGRESS
53-3252
IN PROGRESS
53-3255
IN PROGRESS
53-3256
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FUSELAGE - CENTER
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT
BETWEEN FR53.6-FR53.7
FOR EMERGENCY DOOR
TYPE 1 AREA
CENTER FUSELAGE REINFORCE
CIRCUMFERENTIAL JOINT
BETWEEN FR53.6 FR53.7LH/RH OF OPTION
EMERGENCY DOOR TYPE A
AREA
FUSELAGE-CENTER
FUSELAGE-IMPROVE
FATIGUE LIFE OF INTERNAL
FUSELAGE STRUCTURE ON
LONGITUDINAL BEAMS
ABOVE CENTER WING BOX
CENTER FUSELAGE UPDATE LOWER/LATERAL
FRAME SPLICING WITH
CORNER FITTING BETWEEN
FR53.3 AND FR54
FORWARD FUSELAGE REINFORCE
CIRCUMFERENTIAL JOINT AT
FR 31 BETWEEN STRINGER
7LH AND STRINGER 8RH
FUSELAGE - FORWARD
FUSELAGE - REINFORCE
FRAME COUPLINGS IN
SECTION 13, 14 AND 14A
FUSELAGE - CENTER
FUSELAGE - IMPROVE
ROD/FLOOR ATTACHMENT
FITTING FROM FR53.3 TO
FR54
FORWARD FUSELAGE REINFORCE
CIRCUMFERENTIAL
JOINT/STRINGER COUPLING
IN AREA OF FR37.1
FORWARD FUSELAGE REINFORCE
CIRCUMFERENTIAL
JOINT/STRINGER COUPLING
IN AREA OF FR37.1
FUSELAGE - REAR
FUSELAGE - REINFORCE
STRINGER COUPLINGS AND
CIRCUMFERENTIAL JOINT IN
AREA OF FR76
FUSELAGE - REAR
FUSELAGE - REINFORCE
STRINGER COUPLINGS AND
CIRCUMFERENTIAL JOINT IN
AREA OF FR72
Service Bulletin
Page 18
MAINTENANCE PLANNING DOCUMENT
SB
Number
53-3257
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
53-3258
IN PROGRESS
53-3259
IN PROGRESS
53-3260
IN PROGRESS
53-3263
IN PROGRESS
53-3264
IN PROGRESS
53-3266
IN PROGRESS
53-3273
IN PROGRESS
53-3288
IN PROGRESS
53-3289
IN PROGRESS
53-3291
IN PROGRESS
54-3002
IN PROGRESS
54-3005
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
FUSELAGE - REAR
FUSELAGE - REINFORCE
FRAME COUPLINGS IN REAR
FUSELAGE AREA
FUSELAGE - FORWARD
FUSELAGE - REINFORCE
CORNER FITTINGS IN
SECTION 13
FUSELAGE - REAR
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT AT
FR58 (A/C POST MOD 40556
D18255)
FUSELAGE - REAR
FUSELAGE - REINFORCE
FRAME COUPLINGS FROM
FR60 TO FR64 BETWEEN
STGR 20RH AND STGR 23RH
REAR FUSELAGE REINFORCE FRAMES IN
REAR FUSELAGE AREA
FUSELAGE - FORWARD
FUSELAGE - INSTALL
REINFORCEMENTS AT
FRAME SHELL CORNERS OF
DOOR 2
FUSELAGE - REAR
FUSELAGE - REINFORCE
FRAMES IN AREA OF FR55FR57 BETWEEN STGR22 AND
STGR28 RH/LH
FUSELAGE - CENTER
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT
BETWEEN FR53.6-FR53.7 AT
EMERGENCY EXIT DOOR
TYPE 1 AREA
FUSELAGE - REAR
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINTS
AT FR58
FUSELAGE - REAR
FUSELAGE - REINFORCE
STRINGER COUPLINGS AND
CIRCUMFERENTIAL JOINT IN
AREA FR72
FUSELAGE - CENTER
FUSELAGE - REINFORCE
CIRCUMFERENTIAL JOINT
BETWEEN FR53.6 - FR53.7 OF
OPTIONAL EMERGENCY
DOOR TYPE A AREA
NACELLES/PYLONS PYLONS - REPLACE
MATERIAL OF UPPER AND
LOWER SPIGOT FITTINGS.
NACELLES/PYLONS GENERAL - MODIFY
WING/PYLON FILLET.
Service Bulletin
Page 19
MAINTENANCE PLANNING DOCUMENT
SB
Number
54-3022
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
54-3023
IN PROGRESS
54-3024
IN PROGRESS
55-3032
IN PROGRESS
57-3017
IN PROGRESS
57-3032
IN PROGRESS
57-3038
IN PROGRESS
57-3046
IN PROGRESS
57-3048
IN PROGRESS
57-3051
IN PROGRESS
57-3053
IN PROGRESS
57-3055
IN PROGRESS
57-3058
IN PROGRESS
57-3068
IN PROGRESS
57-3087
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
NACELLES/PYLONS - LOWER
FAIRING - MODIFY
STRUCTURE AT LOWER AFT
PYLON FAIRING LEVEL FOR
PW ENGINES
NACELLES/PYLONS REINFORCE BRACKET OF
PRECOOLER COLD AIR DUCT
BRACKET.
NACELLES / PYLONS - PYLON
BOX - REPLACE RIB18 IN
40CDV12 BY RIB18 IN 15, 5PH.
STABILIZERS-ELEVATORINSPECTION AND
REPROTECTION AGAINST
WATER INGRESS
WINGS - CENTER WING MODIFY RIB 1/WING CENTERSPAR ATTACHMENT
FUSELAGE - CENTER
FUSELAGE - MODIFY LOWER
KEEL FITTING AND
FORWARD LOWER SHELL
CONNECTION.
WINGS - FAIRING - MODIFY
THE FAIRING ATTACHMENT
WINGS - CENTER WING REINFORCE KEEL ANGLE OF
FRONT SPAR.
WINGS INBOARD/OUTBOARD FLAP MODIFY GUIDE BUSH OF
FWD TRACK ATTACHMENT
AT TRACKS 3 THRU 5
WINGS - STRUCTURE REPLACE CLEARANCE FIT
BOLTS WITH INTERFERENCE
FIT BOLTS AT CENTER SPAR
/STRINGER 15 JOINT
WINGS - STRUCTURE REPLACE THE
INTERFERENCE FIT BOLTS
AT RIBS 2 - 7
WINGS - MAIN STRUCTURE COLD EXPAND THE WIRE
HARNESS SLOT RIB 4 - 5
INNER REAR SPAR
WINGS-STRUCTUREREPROFILE THE INNER REAR
SPAR UPPER BUILD SLOT
WINGS - INBOARD FLAP INSTALL ADDITIONAL GFRPLAYERS AROUND THE AFT
END OF THE INBOARD FLAP
TRAILING EDGE
WINGS - MAIN STRUCTURE REWORK RIB 6 AND REFUEL
PIPE FASTENER HOLES
Service Bulletin
Page 20
MAINTENANCE PLANNING DOCUMENT
SB
Number
57-3088
REV
Vendor
SB
Number
Incorporation
Status
IN PROGRESS
57-3090
IN PROGRESS
57-3098
IN PROGRESS
57-3102
IN PROGRESS
57-3124
IN PROGRESS
71-3003
IN PROGRESS
71-3009
IN PROGRESS
71-3016
IN PROGRESS
71-3030
IN PROGRESS
71-3032
IN PROGRESS
78-3012
IN PROGRESS
78-3016
IN PROGRESS
ISSUE: JUL 01/21
SB Title
Customer
work order
Embodiment
status
WINGS - MAIN STRUCTURE MODIFY RIB 6 BETWEEN THE
STRINGERS 18 AND 20
WINGS - CENTER FUSELAGE
- MODIFY FASTENERS IN
FR40 KEELBEAM/BOTTOM
SKIN PANEL JUNCTION
AREA.
WINGS - CENTER WING BOX MODIFY FASTENERS
INSTALLATION IN THE
JUNCTION KEEL BEAM
FITTING AT FR.40
WINGS - INBOARD AND
OUTBOARD FLAPS INTRODUCE MODIFIED
SPHERICAL BEARING AT
FLAP TRACK POSITIONS 2, 3
AND 4
MAIN STRUCTURE-MODIFY
GEAR RIB 6 LUG BORE WITH
IMPROVED BUSH
INSTALLATION
POWER PLANT - COWLING INCREASE CLEARANCE
BETWEEN T/R COWL AND
HYDRAULICACTUATOR
SUPPORT HOUSING
POWER PLANT - ATTACH
FITTINGS - CHANGE FWD
MOUNT BOLT MATERIAL FOR
PW 4164/68.
POWER PLANT - MOUNTS REINFORCE SECONDARY
THRUST LOAD PATH MONOBALL HOUSING ON
A330 P & W FORWARD
MOUNTS.
POWER PLANT - AIR INTAKE
COWL - IMPROVE INTAKE
ACOUSTIC PANEL ON RRTRENT700 ENGINES
POWER PLANT - AIR INTAKE
COWL - INTRODUCE
IMPROVED INTAKE PRIMARY
STRUCTURE AND PICCOLO
TUBE ON RR T700 ENGINE
EXHAUST - THRUST
REVERSER STRUCTURE INTRODUCE A REINFORCED
T/R AFT CASCADE SUPPORT
RING ON PW 4164/68
EXHAUST COLLECTOR/NOZZLE REINFORCE COMMON
NOZZLE ASSEMBLY (CNA)
PAN JUNCTION AREA.
Service Bulletin
Page 21
MAINTENANCE PLANNING DOCUMENT
SB
Number
92-3046
REV
Vendor
92-3062
ISSUE: JUL 01/21
SB
Number
Incorporation
Status
IN PROGRESS
IN PROGRESS
SB Title
Customer
work order
Embodiment
status
ELECTRIC/ELECTRONIC
COMMON INSTALLATIONTHSA - INSTALL ADDITIONAL
HARNESS FOR SECONDARY
NUT DETECTION DESIGN
ELECTRIC AND ELECTRONIC
COMMON INSTALLATION GENERAL - IMPROVE
ELECTRICAL BONDING OF
THE SHIELDED HARNESSES.
Service Bulletin
Page 22
MAINTENANCE PLANNING DOCUMENT
2- SYSTEM S, APU
ANDPOW ERPLAN
T
INTRODUCTION
1. GENERAL
This section provides the scheduled maintenance tasks and frequencies for all Systems, Power Plants
and Auxiliary Power Unit.
Shop maintenance tasks (off-aircraft) may not be included.
With respect to the evaluation procedures and the resulting tasks the following is noted:
1. Operational checks were not considered as forming part of Normal Operating Crew Duties when
determining the evident or hidden aspects of functional failures (ref. Policy and Procedures Handbook
(PPH) para 4.4.4.1).
As a result some tasks given in this section may be considered as flight crew tasks in accordance with
Note 5.
2. deleted in Revision 26
3. Cat II/Cat III landing capabilities, Reduced Vertical Separation Minima (RVSM) capabilities and
Extended Twin Engine Operations (ETOPS) are inherent functions of the basic design standard of the
aircraft. Scheduled tasks necessary for these operations have been considered in the development of
this section. Operators should comply with National Requirements as applicable.
4. Lubrication requirements specified in this MPD do not represent the total lubrication provisions for the
aeroplane. Accordingly, operators should refer to the manufacturer’s appropriate maintenance
publications for additional lubrication information.
5. During the review of an aircraft system for the purpose of modifying or verifying the maintenance
requirements, the reviewer must be aware that those functions associated with the ignition prevention
features of all systems are identified and analyzed in MSI 28-18-00 Ignition Prevention. Any review of
an existing MPD task must therefore consider that it may be necessary to review MPD 281800 in
addition to the specific system MSI identified.
6. Operators should take the opportunity of APU/Power Plant removal and disassembly to perform "offwing" inspections and parts/assemblies restoration as per engine shop manuals. No scheduled basis
for these tasks is defined in this MPD.
7. No threshold or opportunity inspection requirements are given for APU/Power Plant. Manufacturer
may recommend such inspections in the event that late development or early in-service experience
would indicate the desirability to examine specific components of individual engines or APU. If this is
necessary, then direct negotiations between applicable operators and the APU/engine manufacturer
will be arranged. Results of these inspections are to be made available by the manufacturer to other
customer airlines as well as the Regulatory Authorities.
8. Limitations of life limited parts of the APU are controlled and published in GTCP 331-350 (c) Engine
Component Maintenance Manual.
9. APU task intervals quoted in terms of APU HRS may be converted to another usage parameter in
accordance with an appropriate conversion factor based on an operator's specific APU utilization.
10. No recommendation is made for scheduled fuel analysis. Operators who suspect the quality of their
fuel supplies or who operate in an environment known to promote microbiological growth are
recommended to introduce fuel sampling and consider the use of additives to minimize the potential
for such growth.
11. As noted in MRBR Section B, General Rule 6, limitations of life limited parts are controlled by the
manufacturers and published in the following documents:
ISSUE: JUL 01/21
SYSTEMS, APU AND POWER PLANT
Page 1
MAINTENANCE PLANNING DOCUMENT
– Airbus A330 Airworthiness Limitation Section – Part 1, 4 and 5
– GE CF6-80E1 Engine Shop Manual Chapter 5
– PW 4000 Engine Shop Manual Chapter 5
– RR Trent 700 Time Limits Manual, T-Trent-1RR
– RR Trent 7000 Time Limits Manual, ‘T-T7000-1RR’
12. Unless reviewed by Airbus throughout the MSG3 process, maintenance task recommendations
included in Engine Manufacturer documentations such as CESM (GE), MAN (PW), MPG (PW) and
EMP (RR) are not systematically included in the MPD.
13. Tasks approved from Fuel Tank Safety (FTS) Requirements using the criteria established in Special
Federal Aviation Regulation (SFAR88) / EASA policy statement on the process for developing
instructions for maintenance and inspection of fuel tank system ignition source prevention; are
identified with (SFAR88) in parenthesis following the task description in the MPD. This policy has
been applied to Systems & Power Plant tasks listed under ATA 281800 in Section 2.
For Operators under U.S. FAA Jurisdiction only:
Operators requesting revisions to the baseline FTS requirements for failure effect category (FEC) 5
and 8 tasks, description or intervals, must submit their request through the cognizant Flight Standards
District Office, who may add comments and then forward it to the manager of the appropriate FAA
Aircraft Certification Office, or office of the Transport Airplane Directorate, having cognizance over the
type certificate for the affected airplane for concurrence prior to approval. Tasks and intervals other
than FEC 5 and 8 may be revised through normal operator approval process.
For Operators Not under U.S. FAA Jurisdiction:
Operators requesting revisions to the baseline FTS requirements may revise these tasks and intervals
through their normal operator approval process.
14. Electrical Wiring Interconnection System (EWIS) tasks derived from the Enhanced Zonal Analysis
Procedure (EZAP) in ATA 20 of Section Systems, Power Plants and Auxiliary Power Unit and
standard zonal tasks with EWIS content are identified by (EWIS) in parenthesis following the task
description in the MPD.
For Operators under U.S. FAA Jurisdiction only: Operators requesting revisions to the baseline EWIS
task or description must submit their request through the cognizant Flight Standards District Office,
who may add comments and then forward it to the manager of the appropriate FAA Aircraft
Certification Office, or office of the Transport Airplane Directorate, having cognizance over the type
certificate for the affected airplane for concurrence prior to approval. Task intervals may be revised
through normal operator approval process. Tasks indicated with “(EWIS)” after the task description
must not be deleted from the operator's maintenance program.
For Operators not under U.S. FAA Jurisdiction: Operators requesting revisions to the EWIS
requirements may revise these tasks and intervals through their normal operator approval process.
Tasks indicated with “(EWIS)” after the task description must not be deleted from the operator's
maintenance program.
15. Tasks arising from the Enhanced Zonal Analysis Procedure (EZAP), (comprised of GVI tasks not fully
covered by Zonal tasks and DI/RS tasks) are included within ATA chapter 20 of the System and
Powerplant section of the MRBR and have no Failure Effect Category (FEC) quoted. The tasks are
identified with “(EWIS)” following the task description (see “Electrical Wiring Interconnection System
(EWIS)” for further details). These tasks remain under the responsibility of the Zonal Maintenance
Working Group.
NOTE (i): The term “EWIS” in the task description of ATA 20 tasks includes all electrical wiring and
interconnection systems installations (e.g. cables, conduits, clamps, etc…).
NOTE (ii): ATA 20 tasks must not be deleted from the operators maintenance program
NOTE (iii): For advice on cleaning contaminated wiring, refer to the Airbus Electrical Standard
Practices Manual (ESPM) chapter 20-55-20 “CLEANING OF WIRES (Airbus)”.
ISSUE: JUL 01/21
SYSTEMS, APU AND POWER PLANT
Page 2
MAINTENANCE PLANNING DOCUMENT
16. ETOPS capability is included in the A330 certification basis. As a result, the ETOPS particularities
have been considered in the development of the System MSG3 analyses. The basis for ETOPS
consideration in the A330 MRB Report development process is the ETOPS Significant System List.
This provides the list of systems, functions and corresponding rationales established during ETOPS
Certification activities. A system is qualified as “ETOPS significant” when it has a "unique” influence
for ETOPS, in the sense that it specifically participates to the ETOPS basic tenet: "Preclude and
protect the diversion". An ETOPS significant system is either a system having a functional failure that
may contribute to a decision to divert or a system which is has increased importance to ensure a safe
flight and landing following a diversion longer than 60 minutes. Systems that are necessary for the
safe conclusion of all diversions are not considered as ETOPS significant.
Those tasks that result from the functional failure analysis of an ETOPS significant system are
highlighted in this MPD with the words “ETOPS Relevant Task” in the Maintenance Task descriptions
and are applicable to all type of operations (ETOPS Flights and Non-ETOPS Flights).
Operators should also refer to the A330 ETOPS CMP Document (Configuration, Maintenance,
Procedure and Dispatch standards for Extended Diversion Time Operations) for additional ETOPS
Requirements.
ISSUE: JUL 01/21
SYSTEMS, APU AND POWER PLANT
Page 3
MAINTENANCE PLANNING DOCUMENT
2. SECTION NOTES
NOTE 1 to 9
and 11 to 28:
NOTE 10:
The content of these MRBR Section C Notes is given as full text in the
corresponding MPD task.
Operationally check the slide/raft in accordance with the following schedule:
DOOR/EXIT
(RH OR LHSIDE)
QUANTITY
CHECK
(PER
INTERVAL
OPERATORFLEET)
FWD Passenger/Crew Door
1
36 MTHS
MID Passenger/Crew Door
1
36 MTHS
AFT Passenger/Crew Door
1
36 MTHS
Emergency Exit
1
36 MTHS
Checks may be performed on either side and do not all have to be performed on the
same aircraft. As an ongoing continuous maintenance program the operator should
continue the operational check sequence until this schedule has been revised by the
MRB.
Inadvertent deployments may not be used to satisfy the above requirements.
A330 / A340 fleets can be combined for common doors.
For A330-200F applicable for FWD Passenger/Crew Door only.
NOTE 29:
ISSUE: JUL 01/21
Interval to be managed at component level.
Tasks identified with Note 29 in the MRBR are to be managed at component level. In
these cases, the interval is to be counted from the manufacturing date of the
component or from date of previous task accomplishment on the component. Where
an expiry date is applied by the vendor, the operator may seek agreement from local
NAA to change the expiry date to reflect the task interval and thus avoid giving the
impression that the component has been left in service beyond the approved period.
The requirement to manage intervals at component level does not necessarily lead
to serialization of these components. Other means such as electronic tagging or bar
coding may be used as an alternative
SYSTEMS, APU AND POWER PLANT
Page 4
MAINTENANCE PLANNING DOCUMENT
TASK NUMBER
200001-01-1
ZONE
522 LIGHTNING/HIRF PROTECTION-WING
EL
CHK
622
SECURITY CHECK OF THE FOLLOWING HARNESSES END
FITTINGS, FROM RIB 9 TO RIB 10A :
- 7021VP, 7001VC-A, 7021VC-A, 7025VC-A, 10HA1, LH
SIDE
- 7024VP, 7022VC-A, 7026VC-A, 10HA2, RH SIDE
ACCESS: 454BL
464BL
200001-03-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
522AB
622AB
I:
72 MO
SOURCE
REFERENCE
MRB L/HIRF 249200-210-801
MRB REFERENCE:
20-00-01-1
522BB
622BB
633 LIGHTNING/HIRF PROTECTION-WING
EL
CHK
I:
48 MO
MRB L/HIRF 249200-210-816
SECURITY CHECK OF THE CONNECTORS LOCATED ON THE RAT
523 LIGHTNING/HIRF PROTECTION-WING
EL
GVI
623
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES END FITTINGS FROM WING TIP TO RIB
39:
- 7621VB, 7623VB, 7625VB, 7627VB, LH SIDE
- 7622VB, 7624VB, 7626VB, 7628VB, RH SIDE
ACCESS: 523NB
623NB
200001-05-1
535AB
635AB
I:
24 MO
MRB L/HIRF 249200-210-804
I:
48 MO
MRB L/HIRF 249200-210-805
MRB REFERENCE:
20-00-01-5
PREP.: FIXED FLAP TRACK FAIRING Z533;
FIXED FLAP TRACK FAIRING Z633;
FLAPS EXTENDED;
MOVABLE FLAP TRACK FAIRING Z533;
MOVABLE FLAP TRACK FAIRING Z633;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
0.10 ALL
0.10
*
*
0.80
0.80
1
0.05 ALL
*
0.60
1
1
0.40 ALL
0.40
*
*
1.90
1.90
1
1
1
1
0.15 ALL
0.15
0.15
0.15
APPLICABILITY
MRB REFERENCE:
20-00-01-4
575DB
675DB
533 LIGHTNING/HIRF PROTECTION-WING
EL
GVI
574
633 GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
674 FOLLOWING HARNESSES END FITTINGS, FROM RIB 19 TO RIB
14:
- 7633VB LH SIDE
- 7634VB RH SIDE
M/H
MRB REFERENCE:
20-00-01-3
PREP.: RAT EXTENDED;
200001-04-1
MEN
*
12.52
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200001-05-1
ZONE
MEN
M/H
*
*
1.00
1.00
1
1
0.40 PRE
0.40
PREP.: FLAPS EXTENDED;
MOVABLE FLAP TRACK FAIRING Z531;
FLAPS EXTENDED;
MOVABLE FLAP TRACK FAIRING Z631;
*
4.02
*
4.02
ACCESS: 573BB
673BB
*
*
1.15
1.15
1
1
0.30 ALL
0.30
*
0.80
1
1
0.40 POST 43165
0.40
*
4.02
*
4.02
* * * * *
ACCESS: 574CB
674CB
200001-06-1
200001-08-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
574DB
674DB
574EB
674EB
REFERENCE
574FB
674FB
DET
I:
36 MO
MRB L/HIRF 249200-210-806
573DB
673DB
571 LIGHTNING/HIRF PROTECTION-WING
EL
GVI
671
GENERAL VISUAL INSPECTION OF THE FOLLOWING BRAIDED
CONDUIT END FITTINGS, FROM RIB 6 TO FUSELAGE :
- 112QA1-A, 121QA1-A, 122QA1-A, LH SIDE
- 112QA2-A, 121QA2-A, 122QA2-A, RH SIDE
531 LIGHTNING/HIRF PROTECTION-WING
EL
631
DETAILED INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES END FITTINGS, FROM RIB 8 TO
FUSELAGE :
- 7633VB, 7645VB, 7651VB, LH SIDE
- 7634VB, 7646VB, 7652VB, RH SIDE
I:
48 MO
MRB L/HIRF 249200-210-808
MRB REFERENCE:
20-00-01-8
DET
I:
48 MO
MRB L/HIRF 249200-210-821
MRB REFERENCE:
20-00-01-9
PREP.: FLAPS EXTENDED;
MOVABLE FLAP TRACK FAIRING Z531;
FLAPS EXTENDED;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
43165
MRB REFERENCE:
20-00-01-6
PREP.: FUEL PUMP FAIRINGS Z500;
FUEL PUMP FAIRINGS Z600;
200001-09-1
APPLICABILITY
* * * * *
531 LIGHTNING/HIRF PROTECTION-WING
EL
631
DETAILED INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES END FITTINGS, FROM RIB 6 TO
FUSELAGE :
- 7651VB, 7681VB, 7683VB, LH SIDE
- 7652VB, 7682VB, 7684VB, RH SIDE
573CB
673CB
SOURCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200001-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
*
*
1.15
1.15
1
1
1
1
0.50 PRE 53665
0.50 (92-3062)
0.50
0.50
PREP.: WING FILLET FAIRINGS Z191;
WING FILLET FAIRINGS Z192;
*
*
1.00
1.00
ACCESS: 521AB
621AB
*
*
0.40
0.40
1
0.05 ALL
*
0.01
1
1
0.19 ALL
0.19
*
0.02
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
MOVABLE FLAP TRACK FAIRING Z631;
ACCESS: 573BB
673BB
200001-14-1
200002-01-1
573CB
673CB
573DB
673DB
147 LIGHTNING/HIRF PROTECTION- WING
EL
FNC
148
191 FUNCTIONAL CHECK OF THE FOLLOWING WING PRESSURE SEAL
192 BONDINGS: 3502VP, 3504VP, 3506VP, 3508VP, 3514VP,
3501VP, 3503VP, 3505VP, 3507VP, 3513VP, 3722VP,
3736VP, 3738VP, 3744VP, 3721VP, 3735VP, 3737VP,
3743VP
310 LIGHTNING/HIRF PROTECTION-REAR FUSELAGE
SECTION
EL
CHK
I:
72 MO
MRB L/HIRF 249200-210-819
MRB REFERENCE:
20-00-01-14
I:
48 MO
MRB L/HIRF 249200-210-809
MRB REFERENCE:
20-00-02-1
SECURITY CHECK OF THE FOLLOWING HARNESSES END
FITTINGS AT FR.87 :
- 1CS-G, 1CS-H
ACCESS: 312AR
200002-02-1
313 LIGHTNING/HIRF PROTECTION-REAR FUSELAGE
314 SECTION
EL
FNC
I:
72 MO
MRB L/HIRF 249200-210-866
MRB REFERENCE:
20-00-02-2
FUNCTIONAL CHECK OF THE BONDING OF THE FOLLOWING
BRAIDED CONDUITS: 4500VB, 4501VB, 4504VB, 4505VB,
4508VB, 4509VB - LH 4502VB, 4503VB, 4506VB, 4507VB,
4510VB - RH
ACCESS: 313AL
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200002-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
311 LIGHTNING/HIRF PROTECTION-TAIL CONE
EL
312
FUNCTIONAL CHECK OF THE BONDING OF THE FOLLOWING
BRAIDED CONDUITS: 5865VB, 5867VB, 5869VB
FNC
I:
72 MO
SOURCE
REFERENCE
MRB L/HIRF 249200-210-867
200003-01-1
191 LIGHTNING/HIRF PROTECTION-BELLY FAIRING
EL
GVI
I:
48 MO
MRB L/HIRF 249200-210-810
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES END FITTINGS, FROM FR.39 TO
FR.40.2 :
- 1541VB, 1543VB
ACCESS: 191FB
200003-03-1
FNC
I:
72 MO
MRB L/HIRF 249200-210-820
MRB REFERENCE:
20-00-03-3
ACCESS: 191CB
192CB
198GB
200004-01-1
454 LIGHTNING/HIRF PROTECTION-ENGINE PYLON
EL
GVI
464
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
HARNESSES END FITTINGS, FROM RIB 10 TO TEE.
ACCESS: 454BR
464BR
200005-01-1
I:
48 MO
MRB L/HIRF 249200-210-811
1
1
0.10 ALL
0.10
*
0.01
1
0.40 ALL
*
3.70
1
1
1
0.15 PRE 53665
0.15 (92-3062)
0.15
*
*
*
2.50
2.25
1.60
1
1
0.25 ALL
0.25
*
*
0.30
0.30
1
1
0.15 ALL
0.15
MRB REFERENCE:
20-00-04-1
454NR
464NR
731 LIGHTNING/HIRF PROTECTION-MLG
EL
CHK
741
SECURITY CHECK OF THE END FITTINGS AT MLG BRAIDED
CONDUIT.
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
APPLICABILITY
MRB REFERENCE:
20-00-03-1
191KB
191 LIGHTNING/HIRF PROTECTION-BELLY FAIRING
EL
192
198 FUNCTIONAL CHECK OF THE FOLLOWING BELLY FAIRING
PRESSURE SEAL BONDING:
- 3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VP
M/H
MRB REFERENCE:
20-00-02-3
ACCESS: 312AR
R
MEN
I:
48 MO
MRB L/HIRF 249200-210-817
MRB REFERENCE:
20-00-05-1
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200005-02-1
200005-04-1
200006-01-1
200007-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
731 LIGHTNING/HIRF PROTECTION-MLG
EL
DET
741
DETAILED INSPECTION OF ELEMENTS FITTED ON THE ROUTE
2M FROM UNION PLATE TO INTERFACE BRACKET ON STRUT AT
MLG BRAIDED CONDUIT.
I:
731 LIGHTNING/HIRF PROTECTION-MLG
EL
FNC
741
FUNCTIONAL CHECK OF THE BONDING OF BRAIDED CONDUITS
LINKED TO PROXIMITY SENSORS 30GA1, 30GA2, 31GA1,
31GA2.
I:
123 LIGHTNING/HIRF PROTECTION-NLG
EL
711
SECURITY CHECK OF THE FOLLOWING HARNESSES END
FITTINGS AT NLG BRAIDED CONDUIT :
- 1605VC-A, 1607VC-A, 2GH, 1GH
CHK
I:
323 LIGHTNING/HIRF PROTECTION-VERTICAL FIN
GVI
EL
48 MO
SOURCE
MRB L/HIRF 249200-210-813
200007-01-3
312AR
325ML
72 MO
MRB L/HIRF 249200-210-864
EL
48 MO
MRB L/HIRF 249200-210-814
200007-02-2
312AR
325BL
325CL
I:
48 MO
MRB L/HIRF 249200-210-815
EL
GVI
I:
48 MO
MRB L/HIRF 249200-210-815
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
0.15 ALL
0.15
1
1
0.07 ALL
0.07
1
1
0.10 ALL
0.10
1
0.40 A330-200
PRE 49144
*
3.14
1
0.40 A330-300
PRE 49144
*
2.24
1
0.50 A330-200
POST 49144
OR
A330-200F
MRB REFERENCE:
20-00-07-1
GVI
I:
48 MO
MRB L/HIRF 249200-210-815
GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION
INSTALLATION AT VERTICAL FIN:
- 5989VB, 5994VB, 5995VB, 5996VB, 5997VB, 6989VB,
6994VB, 6996VB
* * * * *
1
1
MRB REFERENCE:
20-00-07-1
325DL
323 LIGHTNING/HIRF PROTECTION-VERTICAL FIN
APPLICABILITY
MRB REFERENCE:
20-00-06-1
GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION
INSTALLATION AT VERTICAL FIN:
- 5994VB, 5995VB, 5996VB, 5997VB
ACCESS: 311AZ
M/H
MRB REFERENCE:
20-00-05-4
325NL
323 LIGHTNING/HIRF PROTECTION-VERTICAL FIN
MEN
MRB REFERENCE:
20-00-05-2
GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION
INSTALLATION AT VERTICAL FIN:
- 5994VB, 5995VB, 5996VB, 5997VB
ACCESS: 311AZ
REFERENCE
MRB REFERENCE:
20-00-07-2
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200007-02-2
ZONE
MEN
M/H
*
3.14
1
0.50 A330-300
POST 49144
*
2.24
1
1
1.00 ALL
1.00
PREP.: FLOOR PANELS Z120;
INSULATION Z120;
*
2.00
ACCESS: 131AW
132AZ
*
*
0.25
0.16
1
1
0.15 ALL
0.15
*
0.11
1
1
0.50 ALL
0.50
* * * * *
ACCESS: 311AZ
200007-02-3
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
312AR
325NL
SOURCE
325SL
EL
GVI
I:
48 MO
MRB L/HIRF 249200-210-815
GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION
INSTALLATION AT VERTICAL FIN:
- 5989VB, 5994VB, 5995VB, 5996VB, 5997VB, 6989VB,
6994VB, 6996VB
200121-01-1
200121-02-1
325BL
325CL
MRB REFERENCE:
20-00-07-2
325DL
121 AVIONICS COMPARTMENT
122
CLEANING OF EWIS INSTALLED IN THE AVIONICS
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
AF
RST
I:
72 MO
MRB
249200-100-801
MRB REFERENCE:
20.0.121/01
131BW
132CW
121 AVIONICS COMPARTMENT
AF
GVI
122
GENERAL VISUAL INSPECTION OF 710VU AND 740VU IN THE
AVIONICS COMPARTMENT, (EWIS).
ACCESS: 132AZ
132AZ
200131-01-1
312AR
I:
144 MO
MRB
249200-210-829
MRB REFERENCE:
20.0.121/02
821
821
131 FORWARD CARGO COMPARTMENT
AF
132
CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
RST
I:
72 MO
MRB
249200-100-802
MRB REFERENCE:
20.0.131/01
PREP.: SIDEWALL PANELS Z130;
*
TBD
ACCESS: 821
*
0.10
* * * * *
APPLICABILITY
* * * * *
323 LIGHTNING/HIRF PROTECTION-VERTICAL FIN
ACCESS: 311AZ
REFERENCE
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200131-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
821
200131-03-1
200137-01-1
131 FORWARD CARGO COMPARTMENT
AF
GVI
132
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).
1
1
0.15 ALL
0.15
PREP.: CEILING PANELS Z130;
SIDEWALL PANELS Z130;
*
4.25
ACCESS: 821
821
*
0.10
1
1
0.15 ALL
0.15
*
*
0.55
0.40
2
2
0.25 A330-300
0.25 POST 204025
OR
A330-200
OR
2.00 A330-200F
PRE 58623
0.55 OR
0.55 A330-200F
POST 200281
OR
A330-800
OR
A330-900
137 BAY BEHIND FWD CARGO COMPARTMENT
AF
RST
138
CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD
CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
ACCESS: 131BX
132CX
200141-01-1
200145-01-1
131CX
132DX
131DX
821
I:
144 MO
MRB
249200-210-830
MRB REFERENCE:
20.0.131/02
I:
72 MO
MRB
249200-100-803
MRB REFERENCE:
20.0.137/01
821
141 CENTER WING BOX
AF
GVI
142
GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE
THE FUEL TANK (AS FAR AS VISIBLE), (EWIS).
I:
144 MO
MRB
249200-210-823
MRB REFERENCE:
20.0.141/01
PREP.: FUEL TANK DRAINED AND VENTED;
*
ACCESS: 147AZ
148AZ
*
*
734
744
145 ZONE UNDER CABIN FLOOR
AF
RST
146
CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
I:
144 MO
MRB
249200-100-804
1
1
0.30 ALL
0.30
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200145-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
200151-03-1
200151-04-1
*
98.00
APPLICABILITY
20.0.145/01
PREP.: FLOOR PANELS Z250;
200151-02-1
M/H
* * * * *
FLOOR (ONLY IF CONTAMINATED), (EWIS).
200151-01-1
MEN
151 AFT CARGO COMPARTMENT
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
PREP.: LDMCR (IF INSTALLED);
SIDEWALL PANELS Z150;
*
0.40 A330-300
0.40 WITH LD-MCR
OR
A330-900
WITH LD-MCR
0.01
ACCESS: 822
822
*
0.10
1
1
0.35 A330-200
0.35 WITH LD-MCR
WITHOUT LDL
OR
A330-800
0.01 WITH LD-MCR
WITHOUT LDL
OR
0.10 A330-200F
151 AFT CARGO COMPARTMENT
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
AF
RST
I:
72 MO
MRB
249200-100-805
1
1
MRB REFERENCE:
20.0.151/01
AF
RST
I:
72 MO
MRB
249200-100-805
MRB REFERENCE:
20.0.151/02
PREP.: LDMCR (IF INSTALLED);
SIDEWALL PANELS Z150;
*
ACCESS: 822
822
*
151 AFT CARGO COMPARTMENT
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
AF
RST
I:
72 MO
MRB
249200-100-805
1
1
MRB REFERENCE:
20.0.151/03
PREP.: SIDEWALL PANELS Z150;
*
ACCESS: 822
822
*
151 AFT CARGO COMPARTMENT
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
AF
RST
I:
72 MO
MRB
249200-100-805
MRB REFERENCE:
1
1
0.35 A330-200
0.35 WITHOUT LD-MCR
WITHOUT LDL
OR
A330-800
TBD WITHOUT LD-MCR
WITHOUT LDL
0.10
0.35 A330-200
0.35 WITH LDL
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200151-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
R
200151-09-1
200161-01-1
MEN
M/H
APPLICABILITY
* * * * *
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
200151-05-1
REFERENCE
20.0.151/04
PREP.: LDL (IF INSTALLED);
LDMCR (IF INSTALLED);
SIDEWALL PANELS Z150;
*
ACCESS: 822
822
*
151 AFT CARGO COMPARTMENT
AF
152
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).
1
1
0.15 ALL
0.15
PREP.: CEILING PANELS Z150;
LDL (IF INSTALLED);
LDMCR (IF INSTALLED);
SIDEWALL PANELS Z150;
*
3.51
ACCESS: 822
822
*
0.10
1
1
0.40 A330-300
0.40 WITHOUT LD-MCR
OR
A330-900
WITHOUT LD-MCR
1
1
0.20 A330-200
0.20 OR
A330-300
OR
A330-800
TBD OR
A330-900
0.05
151 AFT CARGO COMPARTMENT
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED),(EWIS).
AF
161 BULK CARGO COMPARTMENT
AF
162
CLEANING OF EWIS INSTALLED IN THE BULK CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
GVI
I:
144 MO
MRB
249200-210-834
A330-200
WITH LDL
0.01 WITH LD-MCR
OR
A330-800
WITH LDL
0.10 OR
A330-800
WITH LDL
WITH LD-MCR
MRB REFERENCE:
20.0.151/05
RST
I:
72 MO
MRB
249200-100-805
MRB REFERENCE:
20.0.151/09
RST
I:
72 MO
MRB
249200-100-816
MRB REFERENCE:
20.0.161/01
PREP.: SIDEWALL PANELS Z160;
*
ACCESS: 823
823
*
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200161-03-1
200161-05-1
200161-06-1
200211-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
161 BULK CARGO COMPARTMENT
AF
162
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).
GVI
I:
144 MO
SOURCE
MRB
REFERENCE
249200-210-835
MEN
1
1
MRB REFERENCE:
20.0.161/02
M/H
APPLICABILITY
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
1.90 OR
A330-900
PREP.: CEILING PANELS Z160;
SIDEWALL PANELS Z160;
*
ACCESS: 823
823
*
0.05
1
1
0.10 A330-200F
0.10
PREP.: CEILING PANELS Z160;
FLIGHT KIT CONTAINER REMOVED, IF INSTALLED;
SIDEWALL PANELS Z160;
*
1.90
ACCESS: 822
822
*
0.10
1
1
0.20 A330-200F
0.20
161 BULK CARGO COMPARTMENT
AF
162
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).
161 BULK CARGO COMPARTMENT
AF
162
CLEANING OF EWIS INSTALLED IN THE BULK CARGO
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
GVI
I:
144 MO
MRB
249200-210-835
MRB REFERENCE:
20.0.161/04
RST
I:
72 MO
MRB
249200-100-816
MRB REFERENCE:
20.0.161/03
PREP.: FLIGHT KIT CONTAINER REMOVED, IF INSTALLED;
SIDEWALL PANELS Z160;
*
TBD
ACCESS: 822
822
*
0.10
1
1
0.20 ALL
0.20
211 COCKPIT
AF
RST
212
CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY IF
CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-806
MRB REFERENCE:
20.0.211/01
PREP.: CEILING PANELS Z210;
FLOOR PANELS Z210;
SIDEWALL PANELS Z210;
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
*
REV. DATE: JUL 01/21
SECTION:
2-20
TBD
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200211-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
211 COCKPIT
AF
GVI
212
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
COCKPIT AT LEVEL OF LATERAL FLOOR STRUCTURE BETWEEN
FR.1 TO FR.11, (EWIS).
I:
144 MO
SOURCE
MRB
REFERENCE
249200-210-836
1
1
*
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
GVI
222
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEATS AND A/C AND SEAT TO SEAT CONNECTION INSTALLED
IN THE FWD CABIN UTILITY AREA, (EWIS).
I:
72 MO
MRB
249200-210-825
MRB REFERENCE:
20.0.221/01
1
1
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND
SEAT TO SEAT CONNECTION, ONLY.
PREP.: SEAT COVERS IF NECESSARY;
200221-02-1
*
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
222
CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
RST
M/H
APPLICABILITY
0.10 ALL
0.10
MRB REFERENCE:
20.0.211/02
PREP.: FLOOR PANELS Z210;
200221-01-1
MEN
I:
144 MO
MRB
249200-100-807
MRB REFERENCE:
1
1
TBD
0.01 A330-200
0.01 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN
UTILITY AREA, SEE
NOTE
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
TBD FORWARD CABIN
UTILITY AREA, SEE
NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN
UTILITY AREA, SEE
NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN
UTILITY AREA, SEE
NOTE
0.30 A330-200
0.30 OR
A330-300
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200221-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
20.0.221/02
PREP.: DOOR FRAME LININGS Z220;
FCRC (IF INSTALLED);
GALLEYS Z220;
INSULATION Z220;
LAVATORIES Z220;
*
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
GVI
222
GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED
IN THE FWD CABIN UTILITY AREA. (EWIS)
I:
144 MO
MRB
249200-210-826
200221-05-1
1
1
MRB REFERENCE:
20.0.221/03
PREP.: DOOR FRAME LININGS Z220;
GALLEYS Z220;
INSULATION Z220;
LAVATORIES Z220;
200221-04-1
M/H
APPLICABILITY
* * * * *
UTILITY AREA (ONLY IF CONTAMINATED), (EWIS).
200221-03-1
MEN
*
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
RST
222
CLEANING OF EWIS INSTALLED IN THE COURIER COMPARTMENT
AREA (ONLY IF CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-824
MRB REFERENCE:
20.0.221/04
1
1
OR
A330-800
39.00 OR
A330-900
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
23.00 OR
A330-900
0.30 A330-200F
0.30
PREP.: DOOR FRAME LININGS Z220;
FCRC (IF INSTALLED);
FLOOR PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
*
52.00
ACCESS: 831
*
0.02
1
1
0.10 A330-200F
0.10
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
GVI
222
GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED
IN THE COURIER COMPARTMENT AREA. (EWIS)
I:
144 MO
MRB
249200-210-862
MRB REFERENCE:
20.0.221/05
PREP.: GALLEYS Z220;
LAVATORIES Z220;
SIDEWALL LININGS Z220;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
*
17.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200221-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
M/H
APPLICABILITY
*
0.02
1
1
0.05 A330-200F
0.05 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
COURIER
COMPARTMENT, SEE
NOTE
* * * * *
ACCESS: 831
200221-06-1
MEN
221 FWD CABIN UTILITY AREA / COURIER COMPARTMENT AF
GVI
222
GENERAL VISUAL INSPECTION OF EWIS CONNECTION,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED
IN THE COURIER COMPARTMENT AREA, (EWIS).
I:
72 MO
MRB
249200-210-825
MRB REFERENCE:
20.0.221/06
NOTE:
TASK ONLY APPLICAPBLE IF SEATS WITH EWIS CONNECTION
BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTIONS
INSTALLED.
200223-01-1
PREP.: SEAT COVERS IF NECESSARY;
*
TBD
ACCESS: 831
*
0.02
223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT /AF
224 COURIER OVERH EAD COMPARTMENT
RST
I:
144 MO
MRB
MRB REFERENCE:
20.0.223/01
CLEANING OF ALL EWIS AND CIRCUIT BREAKERS "5001 VE"
INSTALLED IN THE FWD CABIN UTILITY AREA OVERHEAD
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
200223-02-1
249200-100-808
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
37.70
PREP.: CEILING PANELS Z220;
FCRC (IF INSTALLED);
GALLEYS Z220;
INSULATION Z220;
LAVATORIES Z220;
*
ACCESS: 221AZ
222AZ
*
*
0.27
0.27
1
1
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
221BZ
222BZ
223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT /AF
224 COURIER OVERHEAD COMPARTMENT
GVI
I:
144 MO
MRB
MRB REFERENCE:
20.0.223/02
GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001
VE" AND "G", AND "P"' ROUTES INSTALLED IN THE FWD
CABIN UTILITY AREA OVERHEAD COMPARTMENT, (EWIS).
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
249200-210-827
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200223-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: CEILING PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
*
17.70
ACCESS: 831
*
0.02
1
1
0.15 A330-200F
0.15
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
A330-900
200223-03-1
223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT /AF
224 COURIER OVERHEAD COMPARTMENT
RST
I:
144 MO
MRB
MRB REFERENCE:
20.0.223/03
CLEANING OF ALL EWIS AND CIRCUIT BREAKERS "5001 VE"
INSTALLED IN THE COURIER OVERHEAD COMPARTMENT (ONLY
IF CONTAMINATED), (EWIS).
200223-04-1
PREP.: CEILING PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
*
17.70
ACCESS: 831
*
0.02
1
1
0.10 A330-200F
0.10
223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT /AF
224 COURIER OVERHEAD COMPARTMENT
GVI
I:
144 MO
MRB
249200-210-855
MRB REFERENCE:
20.0.223/04
GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001
VE" AND "G", AND "P" ROUTES INSTALLED IN THE COURIER
OVERHEAD COMPARTMENT AREA, (EWIS).
200230-01-1
249200-100-826
PREP.: CEILING PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
*
17.70
ACCESS: 831
*
0.02
1
2.25 A330-200F
*
2.00
230 FWD MAIN DECK CARGO COMPARTMENT AREA
AF
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE FWD MAIN DECK CARGO
COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).
249200-100-825
MRB REFERENCE:
20.0.230/01
PREP.: SIDEWALL LININGS Z230;
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200230-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
230 FWD MAIN DECK CARGO COMPARTMENT AREA
AF
GVI
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED IN
THE FWD MAIN DECK CARGO COMPARTMENT AREA. (EWIS)
REFERENCE
249200-210-863
231 FWD CABIN
AF
GVI
232
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED
IN THE FWD CABIN AREA, (EWIS).
I:
72 MO
MRB
249200-210-828
0.20 A330-200F
*
2.00
1
1
0.25 A330-200
0.25 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN, SEE
NOTE
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN, SEE
TBD NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN, SEE
NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
FORWARD CABIN, SEE
NOTE
MRB REFERENCE:
20.0.231/01
PREP.: SEAT COVERS IF NECESSARY;
*
231 FWD CABIN
AF
RST
232
CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN AREA
(ONLY IF CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-809
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
MRB REFERENCE:
20.0.231/02
PREP.: FLOOR PANELS Z230;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
* * * * *
APPLICABILITY
1
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR
SEAT TO SEAT CONNECTION, ONLY.
200231-02-1
M/H
MRB REFERENCE:
20.0.230/02
PREP.: SIDEWALL LININGS Z230;
200231-01-1
MEN
*
0.90 A330-200
0.90 OR
A330-300
OR
A330-800
67.00 OR
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200231-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.02
1
1
0.50 A330-200
0.50 OR
A330-300
OR
A330-800
0.80 OR
A330-900
* * * * *
SEATS AND FURNISHINGS Z230;
SIDEWALL LININGS Z230;
ACCESS: 831
200233-01-1
200233-03-1
200240-01-1
233 FWD CABIN OVERHEAD COMPARTMENT
AF
RST
234
CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD
COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-810
MRB REFERENCE:
20.0.233/01
PREP.: CEILING PANELS Z230;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z230;
*
ACCESS: 831
*
0.02
1
1
233 FWD CABIN OVERHEAD COMPARTMENT
AF
GVI
234
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE FORWARD CABIN OVERHEAD COMPARTMENT,
(EWIS).
PREP.: CEILING PANELS Z230;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z230;
*
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
0.80 A330-900
ACCESS: 831
*
0.02
1
0.80 A330-200F
240 FWD MID MAIN DECK CARGO COMPARTMENT
AF
RST
I:
144 MO
MRB
249200-210-857
MRB REFERENCE:
20.0.233/03
I:
144 MO
MRB
CLEANING OF ALL EWIS INSTALLED IN THE FWD MID MAIN
DECK CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED),
(EWIS).
249200-100-827
MRB REFERENCE:
20.0.240/01
PREP.: SIDEWALL LININGS Z240;
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
*
REV. DATE: JUL 01/21
SECTION:
2-20
TBD
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200240-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
240 FWD MID MAIN DECK CARGO COMPARTMENT
AF
GVI
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED IN
THE FWD MID MAIN DECK OVERHEAD CARGO COMPARTMENT
AREA, (EWIS).
200241-01-1
241 MID CABIN UTILITY AREA
AF
GVI
242
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED
IN THE MID CABIN UTILITY AREA, (EWIS).
REFERENCE
249200-210-861
MEN
0.10 A330-200F
1
1
0.01 A330-200
0.01 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN UTILITY
AREA, SEE NOTE
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN UTILITY
TBD AREA, SEE NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN UTILITY
AREA, SEE NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN UTILITY
AREA, SEE NOTE
MRB REFERENCE:
20.0.240/02
I:
72 MO
MRB
249200-210-831
MRB REFERENCE:
20.0.241/01
PREP.: SEAT COVERS IF NECESSARY;
241 MID CABIN UTILITY AREA
AF
RST
242
CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY
AREA (ONLY IF CONTAMINATED), (EWIS).
*
I:
144 MO
MRB
249200-100-811
1
1
MRB REFERENCE:
20.0.241/02
PREP.: FLOOR PANELS Z240;
GALLEYS Z240;
INSULATION Z240;
LAVATORIES Z240;
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
APPLICABILITY
1
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR
SEAT TO SEAT CONNECTION, ONLY.
200241-02-1
M/H
*
REV. DATE: JUL 01/21
SECTION:
2-20
0.25 A330-200
0.25 OR
A330-300
OR
A330-800
42.00 OR
A330-900
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200243-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT AF
244
CLEANING OF ALL EWIS INSTALLED IN THE MID CABIN
UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF
CONTAMINATED), (EWIS).
RST
I:
144 MO
SOURCE
MRB
REFERENCE
249200-100-812
*
243 MID CABIN UTILITY OVERHEAD COMPARTMENT AREA AF
244
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE MID CABIN UTILITY OVERHEAD
COMPARTMENT AREA, (EWIS).
GVI
I:
144 MO
MRB
249200-210-859
MRB REFERENCE:
20.0.243/03
PREP.: CEILING PANELS Z240;
GALLEYS Z240;
LAVATORIES Z240;
200250-01-1
250 MID MAIN DECK CARGO COMPARTMENT AREA
AF
RST
I:
144 MO
MRB
249200-100-821
253 MID MAIN DECK CARGO COMPARTMENT AREA
AF
GVI
254
GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED IN
THE MID MAIN DECK CARGO COMPARTMENT AREA, (EWIS).
I:
144 MO
MRB
249200-210-860
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
APPLICABILITY
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
18.40 A330-900
0.05 A330-200
0.05 OR
A330-300
OR
A330-800
OR
15.40 A330-900
1
1.00 A330-200F
*
4.50
1
1
0.30 A330-200F
0.30
*
4.50
1
1
0.75 A330-200
0.75 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN AREA, SEE
NOTE
MRB REFERENCE:
20.0.250/02
PREP.: SIDEWALL LININGS Z250;
251 MID CABIN
AF
GVI
252
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION,
INSTALLED IN THE MID CABIN AREA. (EWIS).
M/H
MRB REFERENCE:
20.0.250/01
PREP.: SIDEWALL LININGS Z250;
200251-01-1
1
1
*
CLEANING OF EWIS INSTALLED IN THE MID MAIN DECK CARGO
COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).
200250-02-1
1
1
MRB REFERENCE:
20.0.243/01
PREP.: CEILING PANELS Z240;
GALLEYS Z240;
INSULATION Z240;
LAVATORIES Z240;
200243-03-1
MEN
I:
72 MO
MRB
249200-210-832
MRB REFERENCE:
20.0.251/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200251-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
PREP.: SEAT COVERS IF NECESSARY;
*
251 MID CABIN
AF
252
CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA
(ONLY IF CONTAMINATED), (EWIS).
RST
I:
144 MO
MRB
249200-100-813
MRB REFERENCE:
20.0.251/02
PREP.: FLOOR PANELS Z250;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
SEATS AND FURNISHINGS Z250;
SIDEWALL LININGS Z250;
200251-03-1
I:
144 MO
MRB
249200-210-833
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
MRB REFERENCE:
20.0.251/03
PREP.: GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
SEATS AND FURNISHINGS Z250;
C O N T I N U E D
1
1
*
251 MID CABIN
AF
GVI
252
GENERAL VISUAL INSPECTION OF ALL "G" AND "P" ROUTES
INSTALLED IN THE MID CABIN AREA, (EWIS).
* * * * *
APPLICABILITY
* * * * *
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEAT AND AND/OR
SEAT TO SEAT CONNECTION, ONLY.
200251-02-1
M/H
*
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN AREA, SEE
TBD NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN AREA, SEE
NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
MID CABIN AREA, SEE
NOTE
1.00 A330-200
1.00 OR
A330-300
OR
A330-800
>99.9 OR
A330-900
0.20 A330-200
0.20 OR
A330-300
OR
A330-800
34.50 OR
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 19
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200251-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
SIDEWALL LININGS Z250;
200253-01-1
253 MID CABIN OVERHEAD COMPARTMENT
AF
RST
254
CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD
COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-814
MRB REFERENCE:
20.0.253/01
PREP.: CEILING PANELS Z250;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z250;
STAIRHOUSE (IF INSTALLED);
200253-04-1
*
253 MID CABIN OVERHEAD COMPARTMENT
AF
GVI
254
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA,
(EWIS).
I:
144 MO
MRB
249200-210-856
*
260 AFT MID MAIN DECK CARGO COMPARTMENT
AF
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE AFT MID MAIN DECK
CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED),
(EWIS).
249200-100-822
261 AFT CABIN
AF
GVI
262
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED
IN THE AFT CABIN AREA, (EWIS).
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
0.50 A330-200
0.50 OR
A330-300
OR
A330-800
17.40 OR
A330-900
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
17.40 A330-900
1
2.40 A330-200F
*
3.50
1
1
0.50 A330-200
0.50 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN AREA, SEE
NOTE
MRB REFERENCE:
20.0.260/01
PREP.: SIDEWALL LININGS Z260;
200261-01-1
1
1
MRB REFERENCE:
20.0.253/04
PREP.: CEILING PANELS Z250;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z250;
STAIRHOUSE (IF INSTALLED);
200260-01-1
1
1
I:
72 MO
MRB
249200-210-838
MRB REFERENCE:
20.0.261/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 20
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200261-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
PREP.: SEAT COVERS IF NECESSARY;
*
261 AFT CABIN
AF
262
CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA
(ONLY IF CONTAMINATED), (EWIS).
RST
I:
144 MO
MRB
249200-100-817
MRB REFERENCE:
20.0.261/02
PREP.: DOOR FRAME LININGS Z260;
FLOOR PANELS Z260;
GALLEYS (IF INSTALLED);
INSULATION Z260;
LAVATORIES (IF INSTALLED);
SEATS AND FURNISHINGS Z260;
SIDEWALL LININGS Z260;
200263-01-1
I:
144 MO
MRB
249200-100-818
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
MRB REFERENCE:
20.0.263/01
PREP.: CEILING PANELS Z260;
C O N T I N U E D
1
1
*
263 AFT CABIN OVERHEAD COMPARTMENT
AF
RST
264
CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD
COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).
* * * * *
APPLICABILITY
* * * * *
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEATAT AND A/C
AND/OR SEAT TO SEAT CONNECTION, ONLY.
200261-02-1
M/H
*
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN AREA, SEE
TBD NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN AREA, SEE
NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN AREA, SEE
NOTE
0.80 A330-200
0.80 OR
A330-300
OR
A330-800
>99.9 OR
A330-900
0.40 A330-200
0.40 OR
A330-300
OR
A330-800
25.30 OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 21
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200263-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
* * * * *
GALLEYS (IF INSTALLED);
INSULATION Z260;
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z260;
200263-04-1
A330-900
263 AFT CABIN OVERHEAD COMPARTMENT
AF
GVI
264
GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN
THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).
I:
144 MO
MRB
249200-210-858
*
273 AFT MAIN DECK CARGO COMPARTMENT
AF
RST
274
CLEANING OF ALL EWIS INSTALLED IN THE AFT MAIN DECK
CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED),
(EWIS).
I:
144 MO
MRB
249200-100-823
MRB REFERENCE:
20.0.270/01
PREP.: SIDEWALL LININGS Z270;
200271-01-1
1
1
MRB REFERENCE:
20.0.263/04
PREP.: CEILING PANELS Z260;
GALLEYS (IF INSTALLED);
LAVATORIES (IF INSTALLED);
OVERHEAD STOWAGE BINS Z260;
200270-01-1
1
1
*
271 AFT CABIN UTILITY AREA
AF
GVI
272
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN
SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED
IN THE AFT CABIN UTILITY AREA, (EWIS).
I:
72 MO
MRB
249200-210-839
MRB REFERENCE:
20.0.271/01
1
1
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH EWIS
CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT
CONNECTION, ONLY.
PREP.: SEAT COVERS IF NECESSARY;
* * * * *
APPLICABILITY
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
*
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
1.30 OR
A330-900
0.25 A330-200F
0.25
TBD
0.05 A330-200
0.05 IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN UTILITY
AREA, SEE NOTE
OR
A330-300
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN UTILITY
TBD AREA, SEE NOTE
OR
A330-800
IF SEATS WITH EWIS
CONNECTION
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 22
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200271-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
INSTALLED IN THE
AFT CABIN UTILITY
AREA, SEE NOTE
OR
A330-900
IF SEATS WITH EWIS
CONNECTION
INSTALLED IN THE
AFT CABIN UTILITY
AREA, SEE NOTE
200271-02-1
271 AFT CABIN UTILITY AREA
AF
RST
272
CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY
AREA (ONLY IF CONTAMINATED), (EWIS).
I:
144 MO
MRB
249200-100-819
MRB REFERENCE:
20.0.271/02
PREP.: DOOR FRAME LININGS Z270;
FLOOR PANELS Z270;
GALLEYS Z270;
LAVATORIES Z270;
SEATS AND FURNISHINGS Z270;
SIDEWALL LININGS Z270;
200271-03-1
*
271 AFT CABIN UTILITY AREA
AF
GVI
272
GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED
IN THE AFT CABIN UTILITY AREA, (EWIS).
I:
144 MO
MRB
249200-210-840
*
273 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT AF
274
CLEANING OF EWIS AND CIRCUIT BREAKERS "5005 VE"
INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEAD
COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).
RST
I:
144 MO
MRB
249200-100-820
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
MRB REFERENCE:
20.0.273/01
PREP.: CEILING PANELS Z270;
GALLEYS Z270;
* * * * *
1
1
MRB REFERENCE:
20.0.271/03
PREP.: GALLEYS Z270;
INSULATION Z270;
LAVATORIES Z270;
200273-01-1
1
1
*
0.25 A330-200
0.25 OR
A330-300
OR
A330-800
64.20 OR
A330-900
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
36.00 OR
A330-900
0.20 A330-200
0.20 OR
A330-300
OR
A330-800
OR
36.00 A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 23
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200273-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
INSULATION Z270;
LAVATORIES Z270;
200273-02-1
200315-01-1
273 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT AF
GVI
274
GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5005
VE" AND "P" ROUTE INSTALLED IN THE AFT CABIN UTILITY
AREA OVERHEAD COMPARTMENT, (EWIS).
I:
315 TAIL CONE APU AND ACCESSORY COMPARTMENT
AF
GVI
316
GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES
INSTALLED IN THE TAIL CONE FIREWALL AND APU AREA,
(EWIS).
I:
144 MO
MRB
249200-210-841
319 HORIZONTAL STABILIZER CENTER BOX
AF
GVI
54 MO
MRB
249200-210-842
MRB REFERENCE:
20.0.315/01
I:
144 MO
MRB
1
1
0.10 ALL
0.10
*
*
0.04
0.04
2
PREP.: DISCONNECT SCAVENGE WATER SYSTEM PIPE;
FUEL TANK DRAINED AND VENTED;
*
0.40 A330-200
PRE 41600
OR
A330-300
PRE 41600
2.25
ACCESS: 312AR
319CR
*
5.73
2
0.40 A330-200
POST 41600
OR
A330-300
POST 41600
2.25 OR
A330-200F
OR
GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER
CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).
200319-02-1
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
20.0.273/02
ACCESS: 315AL
316AR
200319-01-1
1
1
313AL
319AL
319AR
319BL
319 HORIZONTAL STABILIZER CENTER BOX
249200-210-843
MRB REFERENCE:
20.0.319/01
319BR
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER
CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).
249200-210-843
MRB REFERENCE:
20.0.319/02
PREP.: DISCONNECT SCAVENGE WATER SYSTEM PIPE;
FUEL TANK DRAINED AND VENTED;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
*
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 24
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200319-02-1
ZONE
* * * * *
ACCESS: 312AR
319ER
200333-01-1
200333-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
313AL
319AL
SOURCE
REFERENCE
M/H
APPLICABILITY
* * * * *
319AR
319BL
319DR
*
7.03 A330-800
OR
A330-900
2
2
0.10 ALL
0.10
PREP.: FUEL TANK DRAINED AND VENTED;
*
2.00
ACCESS: 331AT
341AT
*
*
10.90
10.90
333 HORIZONTAL STABILIZER LATERAL BOX
AF
GVI
343
GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER
LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 3 TO
RIB 4 LH/RH, (EWIS).
331BT
341BT
333AB
343AB
333AL
343AR
I:
144 MO
MRB
249200-210-844
MRB REFERENCE:
20.0.333/01
333AT
343AT
333 HORIZONTAL STABILIZER LATERAL BOX
NDT SDI
343
SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER
LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO
RIB 19LH/20RH, (EWIS).
I:
144 MO
MRB
249200-220-801
MRB REFERENCE:
20.0.333/02
PREP.: FUEL TANK DRAINED AND VENTED;
ACCESS: 333BB
343BB
346AB
200333-03-1
MEN
333CB
343CB
333DB
343DB
333EB
343EB
333FB
343FB
333GB
343GB
333 HORIZONTAL STABILIZER LATERAL BOX
NDT SDI
343
SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER
LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO
RIB 14LH/20RH, (EWIS).
I:
144 MO
MRB
249200-220-802
MRB REFERENCE:
20.0.333/03
PREP.: FUEL TANK DRAINED AND VENTED;
ACCESS: 333BB
343BB
346AB
333CB
343CB
333DB
343DB
333EB
343EB
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
343FB
1
1
*
0.60 A330-200
0.60 POST 41471
PRE 43491
OR
A330-300
POST 41471
2.00 PRE 43491
*
*
2.40
3.20
1
1
0.50 A330-200
0.50 PRE 41471
OR
A330-200
POST 43491
PRE 44818
2.00 OR
A330-300
1.60 PRE 41471
3.20 OR
A330-300
POST 43491
PRE 44818
*
*
*
343GB
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 25
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200333-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
333 HORIZONTAL STABILIZER LATERAL BOX
AF
GVI
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER
LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 14 TO
RIB 20LH, (EWIS).
200333-05-1
REFERENCE
249200-210-845
PREP.: FUEL TANK DRAINED AND VENTED;
*
ACCESS: 331ET
*
332AB
332AT
333EL
333 HORIZONTAL STABILIZER LATERAL BOX
NDT SDI
343
SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER
LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO
RIB 20 LH/RH, (EWIS).
ACCESS: 333BB
334AZ
343BB
344GB
I:
144 MO
MRB
249200-220-803
333CB
334GB
343CB
346AB
0.10 A330-200
PRE 41471
OR
A330-200
POST 43491
PRE 44818
2.00 OR
A330-300
16.30 PRE 41471
OR
A330-300
POST 43491
PRE 44818
333EB
333FB
333GB
*
343DB
343EB
343FB
343GB
*
1
1
0.35 TRENT 7000
0.35
*
*
0.10
0.10
2
2
1.10 ALL
1.10
*
4.00
*
I:
24 MO
MRB
249200-210-869
MRB REFERENCE:
20.0.412/01
416AR
426AR
541 INNER FUEL TANK
AF
GVI
641
GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER
FUEL TANK (AS FAR AS VISIBLE), (EWIS).
I:
144 MO
MRB
249200-210-848
MRB REFERENCE:
20.0.541/01
PREP.: FIXED FLAP TRACK FAIRING Z532;
* * * * *
APPLICABILITY
333DB
MRB REFERENCE:
20.0.333/05
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
1
1
M/H
0.70 A330-200
0.70 POST 44818
OR
A330-300
POST 44818
OR
2.10 A330-200F
OR
A330-800
2.95 OR
A330-900
3.60
412 FAN AND ACCESSORY GEAR BOX
AF
GVI
422
GENERAL VISUAL INSPECTION OF EWIS INSTALLED ON THE
FAN AND ACCESSORY GEAR BOX, (EWIS).
ACCESS: 415AL
425AL
200541-01-1
1
MRB REFERENCE:
20.0.333/04
PREP.: FUEL TANK DRAINED AND VENTED;
PEELABLE HOLE COVERS;
200412-01-1
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 26
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200541-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
200542-01-1
541AZ
541DZ
541GZ
541NB
641AZ
641DZ
641GZ
641NB
541BB
541EB
541HB
541PB
641BB
641EB
641HB
641PB
541BZ
541EZ
541JB
541QB
641BZ
641EZ
641JB
641QB
541CB
541FB
541KB
541RB
641CB
641FB
641KB
641RB
541CZ
541FZ
541LB
541SB
641CZ
641FZ
641LB
641SB
542 OUTER FUEL TANK
AF
GVI
642
GENERAL VISUAL INSPECTION OF EWIS IN THE OUTER FUEL
TANK (RIB 23 TO RIB 33)(AS FAR AS VISIBLE), (EWIS).
I:
144 MO
MRB
249200-210-849
200550-01-1
200571-01-1
542BB
542HB
642BB
642HB
542CB
542JB
642CB
642JB
*
4.50
*
16.80
*
16.80
542DB
542KB
642DB
642KB
2
2
0.30 ALL
0.30
*
6.00
542EB
542FB
*
6.50
642EB
642FB
*
6.50
2
2
0.25 ALL
0.25
PREP.: FUEL TANK DRAINED AND VENTED;
*
2.00
ACCESS: 550AB
650AB
*
*
2.25
2.25
1
1
0.15 ALL
0.15
550 VENT SURGE TANK
AF
GVI
650
GENERAL VISUAL INSPECTION OF EWIS WITHIN THE VENT
SURGE TANK (AS FAR AS VISIBLE), (EWIS).
550BB
650BB
I:
144 MO
MRB
249200-210-851
MRB REFERENCE:
20.0.550/01
550CB
650CB
571 MAIN LANDING GEAR WELL
AF
GVI
671
GENERAL VISUAL INSPECTION OF FUEL PUMP EWIS (AS FAR
* * * * *
APPLICABILITY
MRB REFERENCE:
20.0.542/03
PREP.: FIXED FLAP TRACK FAIRING Z534;
FIXED FLAP TRACK FAIRING Z634;
FUEL TANK DRAINED AND VENTED;
ACCESS: 542AB
542GB
642AB
642GB
M/H
* * * * *
FIXED FLAP TRACK FAIRING Z533;
FIXED FLAP TRACK FAIRING Z632;
FIXED FLAP TRACK FAIRING Z633;
ACCESS: 541AB
541DB
541GB
541MB
641AB
641DB
641GB
641MB
MEN
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
I:
144 MO
MRB
249200-210-852
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 27
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
200571-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
*
*
0.40
0.40
APPLICABILITY
20.0.571/01
PREP.: FUEL PUMP FAIRINGS Z500;
FUEL PUMP FAIRINGS Z600;
E N D
M/H
* * * * *
AS VISIBLE), (EWIS).
* * * * *
MEN
* * * * *
SYSTEMS, APU AND POWER PLANT : STANDARD PRACTICES-AIRFRAME
REV. DATE: JUL 01/21
SECTION:
2-20
PAGE 28
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 CABIN AIR DISTRIBUTION AND RECIRCULATION
AF
OPC
I: 20000 FH
SOURCE
MRB 9
OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC
CLOSING OF ISOLATION VALVES OF THE STOWAGE
COMPARTMENT.
212100-02-1
210 CABIN AIR DISTRIBUTION AND RECIRCULATION
AF
REFERENCE
212100-710-802
MEN
M/H
APPLICABILITY
1
0.30 A330-200
POST 46203
1
0.30 A330-200
POST 46201
1
1
1
1
0.20
0.20
0.20
0.20
*
*
*
*
0.15
0.15
0.15
0.15
1
1
0.50 ALL
0.50
MRB REFERENCE:
21.21.00/04
OPC
I:
3200 FH
NOTE
MRB 8
OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC
CLOSING OF ISOLATION VALVES OF THE CREW REST ROOM
(UNDERFLOOR) IN LOWER DECK LAVATORY CONFIGURATION.
212100-710-801
MRB REFERENCE:
21.21.00/05
NOTE:
IF MOBILE CREW REST ROOM IS NOT FITTED WHEN TASK
BECOMES DUE IT MUST BE PERFORMED WHEN MCR IS NEXT
INSTALLED.
212100-03-1
137 CABIN AIR DISTRIBUTION AND RECIRCULATION
CA
DIS
138
145 DISCARD STANDARD RECIRCULATION FILTER ELEMENTS.
146
NOTE:
PLANNING:
- 5600 FH, IF PALL STANDARD RECIRCULATION FILTER
INSTALLED (P/N QB0408-01 AND PREVIOUS)
- 5600 FH, IF LE BOZEC-DONALDSON RECIRCULATION FILTER
INSTALLED (P/N 430B100-2 AMT A, P/N 430B100-3)
- 4000 FH, IF LE BOZEC-DONALDSON RECIRCULATION FILTER
INSTALLED (P/N 430B100-2 AND PREVIOUS).
- CREDIT MAY BE TAKEN FOR MONITORING FILTER CONDITION
THROUGH THE CMS IN ORDER TO MAXIMISE SERVICE LIFE
I:
NOTE
MRB 7
212141-960-801
MRB REFERENCE:
21.21.00/03
ACCESS: 131CX
132CX
151BW
152BW
212100-04-1
137 CABIN AIR DISTRIBUTION AND RECIRCULATION
138
DETAILED INSPECTION OF MIXER UNIT.
AF
DET
I:
4 C
MRB 9
212143-200-801
IF PALL STANDARD
RECIRCULATION
FILTER INSTALLED
OR
IF LE BOZEC
STANDARD
RECIRCULATION
FILTER INSTALLED
MRB REFERENCE:
21.21.00/01
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.30
0.15
1
0.30 IF VCC WITH AIR
FILTER ELEMENT
INSTALLED
1
0.05 IF VCC SMOKE
DETECTION SYSTEM
WITH TEST BUTTON
INSTALLED
1
0.10 IF VCC WITH FAN OFF
SWITCH INSTALLED
1
1
1
1
0.20 IF PALL ODOR
0.20 RECIRCULATION
0.20 FILTER INSTALLED
0.20
*
*
*
*
0.15
0.15
0.15
0.15
* * * * *
ETOPS RELEVANT
ACCESS: 131BX
132CX
212100-06-1
131CX
200 CABIN AIR DISTRIBUTION AND RECIRCULATION
AF
DIS
I:
800 FH
NOTE
MRB 9
DISCARD VIDEO CONTROL CENTER AIR FILTER ELEMENTS.
233653-920-801
MRB REFERENCE:
21.21.00/06
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
212100-07-1
200 CABIN AIR DISTRIBUTION AND RECIRCULATION
EL
OPC
I: 24000 FH
MRB 9
OPERATIONAL CHECK OF "STAND ALONE" SMOKE DETECTION
SYSTEM VIA "SMOKE TEST" BUTTON.
212100-08-1
200 CABIN AIR DISTRIBUTION AND RECIRCULATION
EL
MRB REFERENCE:
21.21.00/07
OPC
I: 24000 FH
MRB 9
OPERATIONAL CHECK OF VCC FAN DEACTIVATION BY USING
THE FAN OFF SWITCH.
212100-14-1
261800-710-805
137 CABIN AIR DISTRIBUTION AND RECIRCULATION
CA
DIS
138
145 DISCARD ODOR RECIRCULATION FILTER ELEMENTS.
146
NOTE:
PLANNING:
- CREDIT MAY BE TAKEN FOR MONITORING FILTER CONDITION
THROUGH THE CMS IN ORDER TO MAXIMISE SERVICE LIFE
212100-710-804
MRB REFERENCE:
21.21.00/08
I:
2400 FH
NOTE
MRB 7
212141-960-805
MRB REFERENCE:
21.21.00/11
ACCESS: 131CX
132CX
151BW
152BW
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212100-16-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 CABIN AIR DISTRIBUTION AND RECIRCULATION
AF
OPC
I:
3200 FH
SOURCE
MRB 8
OPERATIONAL CHECK TO VERIFY CLOSING OF ISOLATION
VALVES OF THE MDCC.
212100-17-1
137 CABIN AIR DISTRIBUTION AND RECIRCULATION
AF
REFERENCE
212100-710-808
OPC
I:
12 YE
OR
34000 FH
MRB 9
212100-710-810
CA
DIS
I:
1200 FH
NOTE
MRB 7
DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT.
152 LAVATORY/GALLEY VENTILATION
AF
1
0.10 A330-200F
1
0.10 A330-200F
*
0.15
DIS
212300-600-801
1
0.80 POST 46135
1
0.30 A330-200
POST 46203
1
0.20 ALL
1
0.50 ALL
MRB REFERENCE:
21.23.00/01
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
212300-02-1
APPLICABILITY
MRB REFERENCE:
21.21.00/14
ACCESS: 131CX
200 LAVATORY/GALLEY VENTILATION
M/H
MRB REFERENCE:
21.21.00/13
OPERATIONAL CHECK OF MORV.
212300-01-1
MEN
I:
DISCARD FILTER ELEMENT.
1200 FH
NOTE
MRB 6
24 MO
MRB 9
212300-600-802
MRB REFERENCE:
21.23.00/02
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
212500-01-1
210 AIR CONDITIONING COMPARTMENT VENTILATION
AF
OPC
I:
OPERATIONAL CHECK OF ABNORMAL VENTILATION WARNING.
212500-02-1
192 AIR CONDITIONING COMPARTMENT VENTILATION
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
AF
DET
212500-710-801
MRB REFERENCE:
21.25.00/01
I:
72 MO
MRB 9
212500-200-801
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212500-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
190 AIR CONDITIONING COMPARTMENT VENTILATION
212600-01-1
192JB
192PB
AF
GVI
I:
48 MO
MRB 9
APPLICABILITY
212500-200-804
193AB
210 AVIONICS EQUIPMENT VENTILATION
AF
210 AVIONICS EQUIPMENT VENTILATION
1
0.30 ALL
*
5.60
1
0.20 ALL
1
0.20 ALL
1
0.10 ALL
1
0.25 ALL
MRB REFERENCE:
21.25.00/03
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING.
212600-02-2
M/H
MRB REFERENCE:
21.25.00/02
GENERAL VISUAL INSPECTION OF PICCOLO TUBES.
ACCESS: 192GB
MEN
* * * * *
DETAILED INSPECTION OF TURBOFAN SUPPLY DUCT.
212500-03-1
REFERENCE
AF
212600-710-805
MRB REFERENCE:
21.26.00/02
73.25.00/01-G6
73.25.00/01-PW
73.25.00/01-RR
OPC
I:
24 MO
OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION.
CMP
MRB 9
212600-710-806
CMP REFERENCE:
21-2-0000-004
MRB REFERENCE:
21.26.00/01
212600-04-1
210 AVIONICS EQUIPMENT VENTILATION
AF
OPC
I: 12000 FH
MRB 8
OPERATIONAL CHECK OF COOLING EFFECT DETECTOR (AEVC
SYSTEM TEST).
212600-07-1
120 AVIONICS EQUIPMENT VENTILATION
AF
RST
212600-710-808
MRB REFERENCE:
21.26.00/04
I:
42 MO
NOTE
MRB 9
CLEANING OF RELAY BOX VU PANELS GRIDS.
122113-100-802
MRB REFERENCE:
21.26.00/06
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212600-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.01
1
0.20 POST 40063
(21-3095)
PRE 51336
(21-3094)
PRE 51337
(21-3093)
1
1
0.20 POST 46386
0.20 (21-3061),
(21-3095)
PRE 51336
(21-3094)
PRE 51337
(21-3093)
1
0.50 ALL
1
0.25 A330-300
POST 40097
(21-3074)
OR
A330-200
POST 45199
(21-3074)
* * * * *
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 132AZ
212700-01-1
210 AVIONICS EQUIPMENT GROUND COOLING
EL
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF FAULT WARNING.
212700-07-1
212800-01-2
212700-710-801
MRB REFERENCE:
21.27.00/01
120 AVIONICS EQUIPMENT GROUND COOLING
210
OPERATIONAL CHECK OF GRU START.
AF
210 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AF
OPC
I:
48 MO
MRB 9
212700-710-803
MRB REFERENCE:
21.27.00/03
OPC
I:
2500 FH
CMP
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF
ISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN
CASE OF SMOKE WARNING.
212800-710-804
CMP REFERENCE:
21-2-0000-001
CMR REFERENCE:
212800-00001-1-C
MRB REFERENCE:
21.28.00/01
26.16.00/02
212800-02-2
210 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AV
OPC
I:
2500 FH
CMP
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD
AIR VALVE IN CASE OF SMOKE WARNING.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
212800-710-805
CMP REFERENCE:
21-2-0000-002
CMR REFERENCE:
212800-00002-1-C
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212800-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
212800-02-4
APPLICABILITY
* * * * *
OR
A330-900
POST 40097
(21-3074)
OR
A330-200F
MRB REFERENCE:
21.28.00/02
R
M/H
210 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AV
OPC
I:
2500 FH
CMP
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD
AIR VALVE IN CASE OF SMOKE WARNING.
212800-710-805
1
0.25 A330-800
POST 45199
(21-3074)
1
0.25 IF LDMCR INSTALLED
1
1
0.40 A330-200
0.40 POST 40379
(25-3168)
PRE 56296
(21-3128)
OR
A330-300
0.10 POST 40379
CMP REFERENCE:
21-2-0000-002
CMR REFERENCE:
212800-00002-1-C
MRB REFERENCE:
21.28.00/02
212800-03-1
210 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AV
OPC
I:
1600 FH
NOTE
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF
LOWER DECK MOBILE CREW REST ISOLATION VALVES IN CASE
OF SMOKE WARNING.
150 LOWER DECK CARGO COMPARTMENT HEATING,
210 VENTILATION AND COOLING (FWD, AFT AND BULK)
EL
OPC
CMR REFERENCE:
212800-00003-1-C
MRB REFERENCE:
21.28.00/03
26.18.00/05
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
212800-04-2
212800-710-806
I:
4 C
MRB 9
212800-710-807
MRB REFERENCE:
21.28.00/04
OPERATIONAL CHECK OF HARD WIRED BACKUP TO VERIFY
CLOSING OF LOWER DECK MOBILE CREW REST ISOLATION
VALVES.
ACCESS: 152VW
* * * * *
*
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212800-04-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
(25-3168)
PRE 56296
(21-3128)
OR
A330-800
POST 40379
(25-3168)
PRE 56296
(21-3128)
OR
A330-900
POST 40379
(25-3168)
PRE 56296
(21-3128)
212800-05-1
210 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AF
OPC
I:
4 C
MRB 9
154 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
AF
DIS
1
0.50 ALL
1
0.30 A330-200
POST 46441
OR
A330-300
POST 46441
OR
A330-800
POST 46441
OR
A330-900
POST 46441
*
0.05
2
1.00 A330-200
POST 46441
OR
MRB REFERENCE:
21.28.00/05
OPERATIONAL CHECK OF HARD WIRED BACKUP OF VENTILATION
CONTROLLER (TO VERIFY CLOSING OF ISOLATION VALVES AND
COLD AIR VALVE).
212800-06-1
212800-710-803
I:
2400 FH
NOTE
MRB 9
212100-960-801
MRB REFERENCE:
21.28.00/06
DISCARD FILTER ELEMENT OF BULK VIDEO COMPARTMENT.
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 823
212800-07-1
154 LOWER DECK CARGO COMPARTMENT HEATING,
VENTILATION AND COOLING (FWD, AFT AND BULK)
EL
OPC
I: 20000 FH
MRB 9
212800-710-809
MRB REFERENCE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
212800-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
21.28.00/07
ACCESS: 823
*
210 PRESSURE CONTROL AND MONITORING
EL
OPC
I: 20000 FH
MRB 8
OPERATIONAL CHECK OF MANUAL MODE.
213100-02-1
210 PRESSURE CONTROL AND MONITORING
AF
OPC
I:
48 MO
OR
24000 FH
MRB 9
210 PRESSURE CONTROL AND MONITORING
AF
OPC
I: 24000 FH
MRB 9
210 PRESSURE CONTROL AND MONITORING
AF
OPC
210 PRESSURE CONTROL AND MONITORING
AF
FNC
270
310 FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P
PROTECTION OF SAFETY VALVES.
I: 24000 FH
MRB 9
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
0.10 ALL
213100-710-803
1
0.10 ALL
213100-710-804
1
0.10 ALL
213100-710-807
1
0.15 ALL
1
1
1
0.30 PRE
0.30
0.30
MRB REFERENCE:
21.31.00/04
I:
6 YE
OR
24000 FH
CMR**
MRB 6,9
NOTE:
THIS TASK MAY BE ALTERNATIVELY ACCOMPLISHED AS AN OFF
AIRCRAFT TASK. REFER TO AMM PROCEDURE FOR REMOVAL AND
* * * * *
1
MRB REFERENCE:
21.31.00/03
OPERATIONAL CHECK OF LANDING FIELD ELEVATION SELECTOR
BY MEANS OF INITIATED TEST (VIA MCDU).
213100-05-1
213100-710-802
A330-300
POST 46441
OR
A330-800
POST 46441
0.05 OR
A330-900
POST 46441
MRB REFERENCE:
21.26.00/03
21.31.00/02
OPERATIONAL CHECK OF OUTFLOW VALVE OPENING (50%) BY
EMERGENCY RAM AIR SWITCH.
213100-04-1
APPLICABILITY
MRB REFERENCE:
21.31.00/01
OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN
DITCHING CONFIGURATION.
213100-03-1
M/H
* * * * *
OPERATIONAL CHECK OF AUTOMATIC AND MANUAL SHUT OFF OF
BULK VIDEO COMPARTMENT VENTILATION AND ELECTRICAL
POWER AND CHECK NON RETURN VALVE IS IN CLOSED
POSITION.
213100-01-1
MEN
213100-720-801
CMR REFERENCE:
213100-00001-2-C
49144
MRB REFERENCE:
21.31.00/05
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
213100-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: ACCESS THROUGH PANEL OF REAR GALLEY;
*
0.75
ACCESS: 312AR
*
0.01
1
1
1
0.30 POST 49144
0.30
0.30
PREP.: ACCESS THROUGH PANEL OF REAR GALLEY;
*
0.75
ACCESS: 312AR
*
0.01
1
0.10 ALL
1
1
0.10 ALL
0.10
*
0.75
1
1
0.40 ALL
0.40
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
INSTALLATION 213152-000-801 AND 213152-400-801
213100-05-2
210 PRESSURE CONTROL AND MONITORING
AF
FNC
270
310 FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P
PROTECTION OF SAFETY VALVES.
I:
6 YE
OR
24000 FH
MRB 6,9
213100-720-801
MRB REFERENCE:
21.31.00/05
NOTE:
THIS TASK MAY BE ALTERNATIVELY ACCOMPLISHED AS AN OFF
AIRCRAFT TASK. REFER TO AMM PROCEDURE FOR REMOVAL AND
INSTALLATION 213152-000-801 AND 213152-400-801
213100-06-1
130 PRESSURE CONTROL AND MONITORING
AF
OPC
I:
4 C
MRB 9
OPERATIONAL CHECK OF NEGATIVE PRESSURE RELIEF VALVE.
213100-07-1
210 PRESSURE CONTROL AND MONITORING
AF
OPC
270
OPERATIONAL CHECK OF POSITION INDICATION OF SAFETY
VALVES.
213100-710-806
MRB REFERENCE:
21.31.00/07
I:
4 C
MRB 9
213100-710-805
MRB REFERENCE:
21.31.00/08
PREP.: ACCESS THROUGH PANEL OF REAR GALLEY;
213100-09-1
210 PRESSURE CONTROL AND MONITORING
270
REMOVE SAFETY VALVE FOR RESTORATION.
AF
RST
I: 50000 FH
OR
12 YE
MRB 9
SEMR
NOTE:
- NO SHORT-TERM EXTENSION IS ALLOWED
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
213152-920-801
MRB REFERENCE:
21.31.00/09
SEMR REFERENCE:
213100-00001-1-E
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
213100-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
210 AIR CONDITIONING (PACKS)
AF
OPC
I: 16500 FH
CMR**
OPERATIONAL CHECK TO VERIFY ABILITY TO SHUT-DOWN BOTH
AIR CONDITIONING PACKS FROM THE FLIGHT DECK.
215000-05-1
APPLICABILITY
*
0.75
190 AIR CONDITIONING (PACKS)
AF
GVI
190 AIR CONDITIONING (PACKS)
AF
DET
215300-710-807
1
0.10 A330-200F
1
0.25 ALL
1
1.00 ALL
*
3.47
1
0.10 POST 40219
(21-3060),
(21-3149)
CMR REFERENCE:
215000-00001-1-C
I: 24000 FH
MRB 9
GENERAL VISUAL INSPECTION OF PACK AIR SUPPLY DUCTS,
CLAMPS AND BELLOWS (BETWEEN PACK OUTLET AND MIXER
UNIT).
215000-06-1
M/H
* * * * *
PREP.: ACCESS THROUGH PANEL OF REAR GALLEY;
215000-01-1
MEN
215200-200-801
MRB REFERENCE:
21.50.00/05
I: 24000 FH
MRB 6,9
DETAILED INSPECTION OF PACK DOWNSTREAM CHECK VALVES
FLAPPERS FOR CONDITION AND OPERATION.
215200-220-801
MRB REFERENCE:
21.50.00/06
NOTE:
ETOPS RELEVANT
ACCESS: 131BX
193BB
215000-07-1
132CX
193CB
132DX
191EB
192GB
192JB
190 FLOW CONTROL AND INDICATING
AF
FNC
I:
8000 FH
NOTE
MRB 9
REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK.
MRB REFERENCE:
21.50.00/08
NOTE:
INTERVAL:
- TO CALCULATE AN OPTIMIZED INTERVAL REFER TO TFU
21.51.00.021.
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
215153-280-801
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215000-11-1
ZONE
190 PACK CONTROL AND INDICATING
AF
FNC
210
FUNCTIONAL CHECK OF RAM AIR INLET DOORS FOR BACKLASH.
ACCESS: 191FB
215000-11-2
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
193BB
* * * * *
193BB
MRB 9
REFERENCE
215300-220-802
MRB REFERENCE:
21.50.00/19
I:
8500 FH
MRB 9
215300-220-802
MRB REFERENCE:
21.50.00/20
193CB
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
3200 FH
193CB
190 PACK CONTROL AND INDICATING
AF
FNC
210
FUNCTIONAL CHECK OF RAM AIR INLET DOORS FOR BACKLASH.
ACCESS: 191FB
I:
SOURCE
MEN
1
1
*
1
1
*
M/H
APPLICABILITY
0.25 A330-200
0.25 PRE 46482
(21-3066)
PRE 46561
2.71 PRE 53111
(21-3111)
OR
A330-300
PRE 46482
(21-3066)
PRE 46561
PRE 53111
(21-3111)
0.25 A330-200
0.25 POST 46482
(21-3066)
OR
2.71 A330-200
POST 46561
OR
A330-200
POST 53111
(21-3111)
OR
A330-300
POST 46482
(21-3066)
OR
A330-300
POST 46561
OR
A330-300
POST 53111
(21-3111)
OR
A330-800
POST 46561
OR
A330-800
POST 53111
(21-3111)
OR
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215000-11-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 46561
OR
A330-900
POST 53111
(21-3111)
215000-12-1
190 AIR CONDITIONING (PACKS)
AF
DIS
I:
REMOVE AND REPLACE THE COMBO SEALS AND PERISEALS ON
THE HOT AIR INLET CIRCUIT, TRIM AIR DUCTING AND PACK
DUCTING.
36 MO
NOTE
MRB 9
215200-920-801
1
15.00 PRE 54523
(21-3115)
OR
PRE 54603
(36-3034)
*
13.50
MRB REFERENCE:
21.50.00/21
NOTE:
- TASK TO PERFORMED PARTIALLY WHERE SILICON SEAL
REMAIN IF ONLY ONE MOD EMBODIED
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S
EXPERIENCE, A LESS OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED
ACCESS: 131BX
192JB
R
215100-01-1
131CX
192PB
132CX
193AB
191DB
193BB
191FB
193DB
192GB
190 FLOW CONTROL AND INDICATING
AF
DIS
I:
2400 FC
NOTE
MRB 7
DISCARD FLOW CONTROL VALVE FILTERS.
215100-920-801
1
0.75 IF P/N 964F0000-XX
INSTALLED
*
2.01
1
1
1.00 ALL
1.00
MRB REFERENCE:
21.50.00/12
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 192JB
R
215200-01-1
193BB
193CB
191 PACK CONTROL AND INDICATING
AF
192
REMOVE REHEATER AND CONDENSER FOR CLEANING AND
LEAKAGE CHECK IN SHOP.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
RST
I: 20000 FH
MRB 9
215200-100-801
MRB REFERENCE:
21.50.00/17
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215200-01-1
ZONE
* * * * *
ACCESS: 193CB
192PB
215300-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
193DB
AF
DET
I:
24 MO
MRB 9
DETAILED INSPECTION OF THE PACK OUTLET DUCTS.
215354-01-1
192JB
MEN
M/H
APPLICABILITY
*
*
2.51
2.00
1
0.50 PRE 48181
(21-3076)
*
3.00
1
1.50 ALL
*
2.70
1
0.10 ALL
1
0.05 ALL
* * * * *
190 PACK CONTROL AND INDICATING
ACCESS: 192GB
REFERENCE
MRB REFERENCE:
21.50.00/22
193BB
190 PACK CONTROL AND INDICATING
215300-220-808
AF
RST
I:
42 MO
NOTE
MRB 7
CLEANING AND DETAILED INSPECTION FOR EROSION OF PACK
WATER INJECTOR NOZZELS.
215300-100-802
MRB REFERENCE:
21.50.00/14
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 191FB
215500-01-1
193BB
210 EMERGENCY RAM AIR INLET
AF
OPC
I: 24000 FH
MRB 9
OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM
OPENING.
215500-710-801
MRB REFERENCE:
21.50.00/02
NOTE:
ETOPS RELEVANT
215500-02-1
190 SKIN CHECK VALVE
AF
DET
DETAILED INSPECTION OF SKIN CHECK VALVE FLAPPERS FOR
CONDITION AND OPERATION.
I:
24 MO
NOTE
MRB 9
215500-200-801
MRB REFERENCE:
21.50.00/15
NOTE:
OPERATORS WITH REGULAR USE OF LP GROUND CARTS ARE
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215500-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
*
0.20
*
0.73
1
0.05 ALL
PREP.: SKIN CHECK VALVE;
*
0.20
ACCESS: 191EB
*
0.02
1
0.05 ALL
PREP.: EMERG RAM AIR INLET CHECK VALVE;
*
0.12
ACCESS: 131CG
*
0.72
1
0.25 A330-200
POST 56732
(47-3002),
(47-3005),
0.01 (47-3008)
PRE 204336
(21-3174)
OR
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
ADVISED TO OPTIMISE THE INTERVAL OF THIS TASK
ACCORDING TO THEIR OPERATING EXPERIENCE. THIS MAY
RESULT IN A LESS OR MORE FREQUENT INTERVAL.
PREP.: SKIN CHECK VALVE;
ACCESS: 131CG
215500-03-1
132AZ
191EB
193CB
190 EMERGENCY RAM AIR INLET
AF
DET
I: 24000 FH
MRB 9
DETAILED INSPECTION OF LP GROUND AIR CHECK VALVE
FLAPPERS FOR CONDITION AND OPERATION.
215500-04-1
215500-220-803
MRB REFERENCE:
21.50.00/04
193CB
190 EMERGENCY RAM AIR INLET
AF
DET
I:
24 MO
NOTE
MRB 9
DETAILED INSPECTION OF EMERGENCY RAM AIR CHECK VALVE
FLAPPERS FOR CONDITION AND OPERATION.
215500-220-804
MRB REFERENCE:
21.50.00/23
NOTE:
OPERATORS WITH REGULAR USE OF LP GROUND CARTS ARE
ADVISED TO OPTIMISE THE INTERVAL OF THIS TASK
ACCORDING TO THEIR OPERATING EXPERIENCE.
THIS MAY RESULT IN A LESS OR MORE FREQUENT INTERVAL.
215800-01-1
191EB
193CB
190 CONDITIONED SERVICE AIR SYSTEM
AF
RST
I:
6000 FH
MRB 9
REMOVE CSAS OZONE CONVERTER FOR IN SHOP CLEANING.
215800-200-801
MRB REFERENCE:
21.58.00/01
ACCESS: 193EB
* * * * *
*
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-21
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215800-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-200
POST 56732
(47-3002),
(47-3005),
(47-3008)
POST 204336
(21-3174)
OR
A330-300
POST 56732
(47-3002),
(47-3005),
(47-3008)
PRE 204337
OR
A330-300
POST 56732
(47-3002),
(47-3005),
(47-3008)
POST 204337
OR
A330-800
POST 56732
(47-3002),
(47-3005),
(47-3008)
POST 204336
(21-3174)
OR
A330-900
POST 56732
(47-3002),
(47-3005),
(47-3008)
POST 204337
215800-02-1
190 CONDITIONED SERVICE AIR SYSTEM
AF
RST
I: 12000 FH
MRB 9
REMOVE CSAS HEAT EXCHANGER FOR IN SHOP CLEANING.
215800-100-801
MRB REFERENCE:
21.58.00/02
ACCESS: 191KB
* * * * *
2
*
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
0.50 A330-200
POST 56732
(47-3002),
(47-3005),
2.00 (47-3008)
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
215800-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-300
POST 56732
(47-3002),
(47-3005),
(47-3008)
OR
A330-800
POST 56732
(47-3002),
(47-3005),
(47-3008)
OR
A330-900
POST 56732
(47-3002),
(47-3005),
(47-3008)
216000-01-1
200 COCKPIT AND CABIN TEMPERATURE CONTROL
AF
RST
I:
CLEANING OF CABIN TEMPERATURE SENSORS, SENSE LINES
AND INLETS.
1600 FH
NOTE
MRB 7
216317-100-801
1
0.50 A330-200
PRE 43750
(21-3046)
PRE 44729
(21-3049)
OR
A330-300
PRE 43750
(21-3046)
PRE 44729
(21-3049)
*
2.28
1
0.80 ALL
*
1.46
MRB REFERENCE:
21.50.00/09
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 232BC
216000-02-1
252EF
262FC
130 COCKPIT AND CABIN TEMPERATURE CONTROL
AF
DET
I:
4 C
MRB 9
DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS
FOR CONDITION AND OPERATION.
ACCESS: 131BX
131CX
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
132CX
191EB
216300-200-801
MRB REFERENCE:
21.50.00/03
193BB
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
216000-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 COCKPIT AND CABIN TEMPERATURE CONTROL
AF
RST
I: 10000 FH
SOURCE
MRB 7
CLEAN FLIGHT DECK TEMPERATURE SENSORS.
216000-05-1
200 COCKPIT AND CABIN TEMPERATURE CONTROL
REFERENCE
216317-100-802
MEN
1
0.30 ALL
AF
DIS
I:
800 FH
NOTE
MRB 7
216317-920-802
1
0.25 A330-200
POST 43750
(21-3046)
OR
A330-200
POST 44729
(21-3049)
OR
A330-300
POST 43750
(21-3046)
OR
A330-300
POST 44729
(21-3049)
OR
A330-800
POST 43750
(21-3046)
OR
A330-900
POST 43750
(21-3046)
1
1
0.50 POST 49520
0.50 (21-3096)
*
*
4.50
3.20
1
1.50 A330-200F
MRB REFERENCE:
21.50.00/10
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
191 PACK CONTROL AND INDICATING
AF
192
GENERAL VISUAL INSPECTION OF HEATSHIELDS FOR
CONDITION AND VISIBLE DAMAGE.
ACCESS: 191KB
192MB
216000-10-1
GVI
I: 24000 FH
MRB 8
MRB REFERENCE:
21.50.00/13
AF
RST
I:
1600 FH
NOTE
MRB 9
CLEANING OF COURIER AREA AND MDCC TEMPERATURE
SENSORS, SENSE LINES & INLETS AND DISCARD OF
TEMPERATURE SENSOR FILTER.
* * * * *
215300-210-801
193DB
192PB
200 COURIER AREA AND MDCC TEMPERATURE CONTROL
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
APPLICABILITY
MRB REFERENCE:
21.50.00/01
DISCARD CABIN TEMPERATURE SENSOR FILTERS.
216000-08-1
M/H
216300-100-802
MRB REFERENCE:
21.50.00/16
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
216000-10-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
0.32
APPLICABILITY
* * * * *
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 221XW
* * * * *
232VW
E N D
SYSTEMS, APU AND POWER PLANT : AIR CONDITIONING
252QX
262SW
272QW
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -21
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
221000-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AUTOPILOT/FLIGHT DIRECTOR
AV
OPC
I:
72 MO
SOURCE
CMP
MRB 9
OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION.
210 AUTOPILOT/FLIGHT DIRECTOR
AV
OPC
I:
72 MO
MRB 9
210 AUTOTHRUST
AV
OPC
I:
72 MO
MRB 9
210 FLIGHT MANAGEMENT (FM)
AV
OPC
I:
48 MO
MRB 9
210 FLIGHT MANAGEMENT (FM)
AV
210 FLIGHT MANAGEMENT
OPC
I:
48 MO
MRB 9
AV
210 FLIGHT MANAGEMENT
OPC
I:
24 MO
MRB 9
0.30 ALL
E N D
SYSTEMS, APU AND POWER PLANT : AUTO FLIGHT
223000-710-801
1
0.30 ALL
227000-710-803
1
0.30 ALL
227000-710-804
1
0.30 ALL
227000-710-802
1
0.10 ALL
1
0.05 ALL
MRB REFERENCE:
22.70.00/02
AV
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF MCDU ANNUNCIATORS.
* * * * *
1
MRB REFERENCE:
22.70.00/01
OPERATIONAL CHECK OF MCDU 3 TRANSFER.
227500-02-1
221000-710-803
MRB REFERENCE:
22.70.00/04
OPERATIONAL CHECK OF BACK-UP NAVIGATION FUNCTION.
227500-01-1
0.10 ALL
MRB REFERENCE:
22.30.00/01
OPERATIONAL CHECK OF FM SOURCE SWITCHING.
227200-01-1
1
APPLICABILITY
MRB REFERENCE:
22.10.00/02
OPERATIONAL CHECK OF A/THR ISOLATION FROM ENGINE
CONTROL.
227100-01-1
M/H
MRB REFERENCE:
22.10.00/01
OPERATIONAL CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING
DEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS.
223100-01-1
221000-710-801
MEN
CMP REFERENCE:
22-2-0000-001
NOTE:
ETOPS RELEVANT
221100-01-1
REFERENCE
227000-710-801
MRB REFERENCE:
22.70.00/03
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -22
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
233300-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
120 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)
EL
DIS
I:
2400 FH
NOTE
SOURCE
MRB 9
DISCARD IFE-RACK FILTER ELEMENTS.
REFERENCE
233300-920-801
ACCESS: 132AZ
*
200 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)
EL
RST
I: 10000 FH
MRB 9
CLEANING OF VENTILATION GRIDS AND VENTILATOR HOUSING
(IF INSTALLED) FROM IFE COMPONENTS INSTALLED IN THE
CABIN (VCC/VCI/RCC).
* * * * *
1
MRB REFERENCE:
23.33.00/02
46.40.01/01
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
233300-03-1
MEN
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
233653-100-801
MRB REFERENCE:
23.33.00/03
1
M/H
APPLICABILITY
0.30 A330-200
IF IFE-RACKS
AIR-FILTERS
INSTALLED
OR
A330-300
IF IFE-RACKS
AIR-FILTERS
INSTALLED
OR
A330-800
0.01 IF IFE-RACKS
AIR-FILTERS
INSTALLED
OR
A330-900
IF IFE-RACKS
AIR-FILTERS
INSTALLED
SECTION:
2 -23
WITH
WITH
WITH
0.50 A330-200
IF VCC INSTALLED
OR
A330-200
IF VCI INSTALLED
OR
A330-200
IF RCC INSTALLED
OR
A330-300
IF VCC INSTALLED
OR
A330-300
IF VCI INSTALLED
OR
A330-300
IF RCC INSTALLED
OR
A330-800
IF VCC INSTALLED
OR
A330-800
IF VCI INSTALLED
OR
* * * * *
REV. DATE: JUL 01/21
WITH
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
233300-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-800
IF RCC INSTALLED
OR
A330-900
IF VCC INSTALLED
OR
A330-900
IF VCI INSTALLED
OR
A330-900
IF RCC INSTALLED
233901-01-1
130 SATELLITE TV TRANSCEIVER SYSTEM TAILWIND
(TW560) AND PANASONIC (IDTV)
EL
DIS
I:
800 FH
MRB 7
210 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION
BY BOEING (CBB)
EL
OPC
I:
4 C
MRB 9
120 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION
210 BY BOEING (CBB)
EL
OPC
I:
4 C
MRB 9
233900-710-816
233900-710-817
MRB REFERENCE:
23.39.02/02
OPERATIONAL CHECK OF COOLING LOSS DETECTION OF
CONNEXION BY BOEING SYSTEM.
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
0.30 A330-200
TAILWIND SYSTEM
INSTALLED
OR
A330-300
TAILWIND SYSTEM
INSTALLED
1
0.10 A330-200
POST 54258
PRE 58645
(23-3251)
OR
A330-300
POST 54258
PRE 58645
(23-3251)
1
1
0.10 A330-200
0.10 POST 54258
PRE 58645
(23-3251)
OR
A330-300
POST 54258
PRE 58645
(23-3251)
MRB REFERENCE:
23.39.02/01
OPERATIONAL CHECK OF CONNEXION BY BOEING SYSTEM POWER
OFF PROCEDURE.
233902-02-1
1
MRB REFERENCE:
23.39.01/01
DISCARD ALL FILTER ELEMENTS ON TAILWIND SYSTEM.
233902-01-1
233900-610-802
REV. DATE: JUL 01/21
SECTION:
2 -23
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
235100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AUDIO MANAGEMENT (INTEGRATING/FLIGHT
INTERPHONE/SELCAL/CALL)
RA
OPC
I:
24 MO
SOURCE
MRB 9
210 AUDIO MANAGEMENT (INTEGRATING/FLIGHT
INTERPHONE/SELCAL/CALL)
AF
OPC
I:
48 MO
MRB 9
236100-02-1
R
237100-01-1
300 STATIC DISCHARGER
RA
500
600 CHECK RESISTANCE FROM THE DISCHARGER TO THE BASE
(RETAINER) AND FROM THE BASE (RETAINER) TO THE
AIRCRAFT STRUCTURE.
FNC
300 STATIC DISCHARGER
AF
500
600 GENERAL VISUAL INSPECTION OF STATIC DISCHARGER.
GVI
210 COCKPIT VOICE RECORDER (CVR)
OPC
RA
I:
24 MO
MRB 9
237100-02-1
210 COCKPIT VOICE RECORDER (CVR)
RA
I:
24 MO
MRB 9
237135-01-1
160 COCKPIT VOICE RECORDER (CVR)
RA
I:
36 MO
MRB 9
OPC
I:
48 MO
MRB 9
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
1
0.30 ALL
2
0.60 ALL
1
1
1
0.25 ALL
0.25
0.25
236100-210-801
1
1
1
0.20 ALL
0.20
0.20
DIS
237100-710-801
1
0.30 PRE
208191
237100-710-802
2
0.30 PRE
208191
1
0.10 PRE
208191
MRB REFERENCE:
23.71.00/02
I:
CE
NOTE
MRB 9
237135-920-801
MRB REFERENCE:
23.71.00/03
NOTE:
INTERVAL:
C O N T I N U E D
APPLICABILITY
MRB REFERENCE:
23.51.00/02
23.71.00/01
DISCARD ULB BATTERY.
* * * * *
236100-200-801
MRB REFERENCE:
23.61.00/02
OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING
TIME DELAY RELAY.
R
235100-710-803
MRB REFERENCE:
23.61.00/01
OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING.
R
M/H
MRB REFERENCE:
23.51.00/03
OPERATIONAL CHECK OF CAPTAIN AND F/O ACP SWITCHING TO
THIRD ACP.
236100-01-1
235100-710-804
MEN
MRB REFERENCE:
23.51.00/01
OPERATIONAL CHECK OF OXYGEN MASK MICROPHONE.
235100-02-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -23
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
237135-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.10
1
0.15 PRE
*
0.10
1
1
0.20 A330-200
0.20 OR
A330-300
OR
A330-800
OR
A330-900
1
0.10 PRE
PRE
OR
PRE
PRE
* * * * *
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 162TW
R
237135-02-1
823
160 COCKPIT VOICE RECORDER (CVR)
AV
OPC
I:
36 MO
MRB 9
OPERATIONAL CHECK OF THE ULB.
ACCESS: 162TW
237300-01-1
237300-02-1
237100-710-804
MRB REFERENCE:
23.71.00/04
823
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) RA
OPC
210
OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY,
DEUS-A CUT OFF FUNCTION.
I: 36000 FH
210 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)
I:
RA
OPC
OPERATIONAL CHECK OF CABIN SIGNS VIA MCDU.
MRB 9
237300-710-808
MRB REFERENCE:
23.73.00/03
2000 FH
NOTE
MRB 9
237300-710-809
MRB REFERENCE:
23.73.00/01
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
237300-03-1
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)
210
OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU.
RA
OPC
I: 12000 FH
NOTE
MRB 9
237300-710-810
MRB REFERENCE:
23.73.00/02
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
208191
1
1
44058
48823
45556
48823
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -23
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
237300-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED.
237300-04-1
237300-05-2
237300-07-1
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)
210
OPERATIONAL CHECK OF EVAC FUNCTION.
EL
OPC
I: 36000 FH
MRB 9
237300-710-804
1
1
0.10 A330-200
0.10 IF EVAC INSTALLED
OR
A330-300
IF EVAC INSTALLED
OR
A330-800
IF EVAC INSTALLED
OR
A330-900
IF EVAC INSTALLED
1
1
0.20 POST 40823
0.20 PRE 49314
1
1
0.10 IF LED SIGNS IN
0.10 LOWER DECK
COMPARTMENTS
INSTALLED
1
1
0.10 POST 50156
0.10 (23-3124)
OR
POST 50157
(23-3124)
MRB REFERENCE:
23.73.00/04
120 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) AV
OPC
200
OPERATIONAL CHECK OF HOT BATTERY BUS POWERED CIDS
OPERATION.
I: 20000 FH
100 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) AV
OPC
210
OPERATIONAL CHECK OF LIGHTED SIGNS IN OPTIONAL LOWER
DECK COMPARTMENTS.
I:
MRB 9
237300-710-815
MRB REFERENCE:
23.73.00/05
4 C
NOTE
MRB 9
237300-710-825
MRB REFERENCE:
23.73.00/08
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
237300-09-1
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) EL
OPC
210
OPERATIONAL CHECK OF EMERGENCY CABIN ALERT SYSTEM
(ECAS).
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
I: 24000 FH
MRB 9
237300-710-818
MRB REFERENCE:
23.73.00/09
REV. DATE: JUL 01/21
SECTION:
2 -23
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
237300-10-1
237301-01-1
237301-02-1
237301-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) EL
210
OPERATIONAL CHECK OF BATTERY POWERED CIDS PA
OPERATION.
OPC
I: 24000 FH
I: 20000 FH
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)
210
OPERATIONAL CHECK OF EVAC FUNCTION.
I: 20000 FH
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) EL
210
OPERATIONAL CHECK OF BATTERY POWERED CIDS PA
OPERATION.
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : COMMUNICATIONS
MRB 9
REFERENCE
237300-710-839
MEN
OPC
MRB 9
237300-710-837
APPLICABILITY
0.10 A330-200
0.10 POST 49314
OR
A330-300
POST 49314
OR
A330-800
POST 49314
OR
A330-900
POST 49314
1
1
0.20 A330-200F
0.20
1
1
0.10 A330-200F
0.10
1
1
0.10 A330-200F
0.10
MRB REFERENCE:
23.73.01/01
MRB 9
237300-710-835
MRB REFERENCE:
23.73.01/02
OPC
M/H
1
1
MRB REFERENCE:
23.73.00/10
200 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) EL
OPC
210
OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, AND
DEUS-A CUT OFF FUNCTION.
EL
SOURCE
I: 20000 FH
MRB 9
237300-710-836
MRB REFERENCE:
23.73.01/03
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-23
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242100-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
FNC
422
CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT.
I:
2100 FH
SOURCE
MRB 9
242100-08-1
416AR
426AR
417AL
427AL
418AR
428AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
DIS
422
DRAIN IDG OIL SYSTEM, DISCARD SCAVENGE FILTER ELEMENT
AND REPLENISH.
T:
150 FH
I:
800 FH
OR
NOTE
CMP
MRB 6
242100-09-1
416AR
426AR
417AL
427AL
121324-612-806
RST
1
1
0.15 GE
0.15
*
*
0.20
0.20
1
1
0.60 GE
0.60
*
*
0.20
0.20
APPLICABILITY
MRB REFERENCE:
24.20.00/05
418AR
428AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
CLEAN (IN SHOP) INTEGRATED DRIVE GENERATOR OIL
COOLERS.
M/H
CMP REFERENCE:
24-2-0000-001
NOTE:
- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH
AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER
TO INTERVAL.
- IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO
NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME
TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO
FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE
OTHER IDG.
- ETOPS RELEVANT
ACCESS: 415AL
425AL
242100-210-807
MEN
MRB REFERENCE:
24.20.00/06
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
REFERENCE
I:
4 C
MRB 6
242142-100-801
0
0
N/A GE
N/A
MRB REFERENCE:
24.20.00/13
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
SHOP VISIT.
OFF A/C TASK
ETOPS RELEVANT
PREP.: REMOVE IDG OIL COOLERS Z412;
REMOVE IDG OIL COOLERS Z422;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
*
*
2.50
2.50
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-24
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242100-09-1
ZONE
* * * * *
ACCESS: 415AL
425AL
242100-10-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
416AR
426AR
417AL
427AL
SOURCE
REFERENCE
MEN
M/H
*
*
0.20
0.20
2
2
0.20 GE
0.20
*
*
0.01
0.01
1
1
0.25 PW
0.25
1
1
0.60 PW
0.60
*
*
0.13
0.13
APPLICABILITY
* * * * *
418AR
428AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR
DISCONNECT FUNCTION.
OPC
I:
72 MO
MRB 9
242100-710-803
MRB REFERENCE:
24.20.00/14
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
OR IDG CHANGE.
ACCESS: 414BL
424BL
242100-12-1
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
FNC
422
CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT.
I:
2100 FH
MRB 9
242100-210-815
MRB REFERENCE:
24.20.00/06
NOTE:
ETOPS RELEVANT
242100-13-1
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
DIS
422
DRAIN IDG OIL SYSTEM, DISCARD SCAVENGE FILTER ELEMENT
AND REPLENISH.
T:
150 FH
I:
800 FH
OR
NOTE
CMP
MRB 6
NOTE:
- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH
AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER
TO INTERVAL.
- IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO
NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME
TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO
FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE
OTHER IDG.
- ETOPS RELEVANT
ACCESS: 415BL
425BL
416BR
426BR
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
417AL
427AL
121324-612-807
CMP REFERENCE:
24-2-0000-001
MRB REFERENCE:
24.20.00/05
418AR
428AR
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242100-14-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
CLEAN (IN SHOP) INTEGRATED DRIVE GENERATOR OIL
COOLERS.
RST
I:
4 C
SOURCE
MRB 6
REFERENCE
242100-100-801
MEN
0
0
M/H
APPLICABILITY
N/A PW
N/A
MRB REFERENCE:
24.20.00/13
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
SHOP VISIT.
OFF A/C TASK
ETOPS RELEVANT
242100-15-1
PREP.: REMOVE IDG OIL COOLERS Z412;
REMOVE IDG OIL COOLERS Z422;
*
*
2.50
2.50
ACCESS: 415BL
425BL
*
*
0.13
0.13
2
2
0.20 PW
0.20
1
1
0.15 TRENT 700
0.15
*
*
0.10
0.10
1
1
0.60 RR
0.60
416BR
426BR
417AL
427AL
418AR
428AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR
DISCONNECT FUNCTION.
OPC
I:
72 MO
MRB 9
242100-710-806
MRB REFERENCE:
24.20.00/14
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
OR IDG CHANGE.
242100-17-1
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
FNC
422
CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT.
I:
2100 FH
MRB 9
242100-210-811
MRB REFERENCE:
24.20.00/06
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
242100-18-1
416AR
426AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
DIS
422
DRAIN IDG OIL SYSTEM, DISCARD SCAVENGE FILTER ELEMENT
AND REPLENISH.
T:
150 FH
I:
800 FH
OR
NOTE
CMP
MRB 6
NOTE:
* * * * *
121324-612-809
CMP REFERENCE:
24-2-0000-001
MRB REFERENCE:
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242100-18-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
242100-19-1
MEN
M/H
*
*
0.10
0.10
APPLICABILITY
* * * * *
- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH
AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER
TO INTERVAL. FOR A330-800 AND A330-900 INTERVAL
CANNOT EXCEED 800FHS.
- IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO
NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME
TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO
FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE
OTHER IDG.
- ETOPS RELEVANT
ACCESS: 415AL
425AL
REFERENCE
24.20.00/05
416AR
426AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
CLEAN (IN SHOP) INTEGRATED DRIVE GENERATOR OIL
COOLERS.
RST
I:
4 C
MRB 6
242142-100-802
0
0
N/A RR
N/A
MRB REFERENCE:
24.20.00/13
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
SHOP VISIT.
OFF A/C TASK
ETOPS RELEVANT
PREP.: REMOVE
REMOVE
REMOVE
REMOVE
ACCESS: 415AL
425AL
242100-20-1
IDG
IDG
IDG
IDG
OIL
OIL
OIL
OIL
COOLERS Z412;
TUBES Z412;
COOLERS Z422;
TUBES Z422;
416AR
426AR
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR
DISCONNECT FUNCTION.
OPC
I:
72 MO
MRB 9
242100-710-808
*
2.75
*
2.75
*
*
0.10
0.10
1
1
0.22 TRENT 700
0.22
MRB REFERENCE:
24.20.00/14
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
OR IDG CHANGE.
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
242100-23-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
412 INTEGRATED DRIVE GENERATOR
AF
FNC
422
CHECK IDG OIL FILTER DIFFERENTIAL PRESSURE INDICATOR
I:
NOTE
SOURCE
CMP
REFERENCE
242151-210-803
ACCESS: 414BL
424BL
412 AC GENERATION
AF
FNC
422
CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT.
I:
1200 FH
MRB 9
242100-210-834
M/H
APPLICABILITY
1
1
0.02 ETOPS
0.02 RR
PRE 43286
(24-3008)
*
*
0.01
0.01
1
1
0.65 A330-800
0.65 OR
A330-900
1
1
1
1
0.10 A330-900
0.10 PRE 209109
0.10
0.10
*
*
*
*
0.05
0.05
0.05
0.05
1
1
0.22 TRENT 7000
0.22
CMP REFERENCE:
24-2-0000-009
NOTE:
- THIS TASK MUST BE PERFORMED BEFORE EACH FLIGHT
242100-24-1
MEN
MRB REFERENCE:
24.20.00/19
NOTE:
ETOPS RELEVANT
R
242100-25-1
415 AC GENERATION
AF
VCK
416
425 VISUAL CHECK OF IDG OIL SIGHT GLASS TO CONFIRM OIL
426 LEVEL IS WITHIN SPECIFIED LIMITS IN ACCORDANCE TO HOT
OR COLD OIL CONDITION.
I:
400 FH
MRB 9
242100-210-831
MRB REFERENCE:
24.20.00/20
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
416AR
425AL
426AR
242100-26-1
412 INTEGRATED DRIVE GENERATOR SYSTEM
EN
422
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR
DISCONNECT FUNCTION.
OPC
I:
72 MO
MRB 9
242100-710-814
MRB REFERENCE:
24.20.00/14
NOTE:
TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE
OR IDG CHANGE.
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
242100-27-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
412 INTEGRATED DRIVE GENERATOR
AF
FNC
422
CHECK IDG OIL FILTER DIFFERENTIAL PRESSURE INDICATOR
I:
NOTE
SOURCE
CMP
REFERENCE
CMP REFERENCE:
24-2-0000-009
MEN
N
242100-28-1
412 INTEGRATED DRIVE GENERATOR
AF
FNC
422
CHECK IDG OIL FILTER DIFFERENTIAL PRESSURE INDICATOR
I:
NOTE
CMP
CMP REFERENCE:
24-2-0000-009
APPLICABILITY
1
1
0.02 ETOPS
0.02 GE
PRE 43286
(24-3008)
*
*
0.01
0.01
1
1
0.02 ETOPS
0.02 PW
PRE 43285
(24-3008)
*
*
0.01
0.01
1
0.15 ALL
1
0.15 NON-ETOPS
OR
EASA
ETOPS
UP TO 180 MIN D.T.
1
0.15 EASA
ETOPS
BEYOND 180 MIN D.T.
NOTE:
- THIS TASK MUST BE PERFORMED BEFORE EACH FLIGHT
ACCESS: 414BL
424BL
M/H
NOTE:
- THIS TASK MUST BE PERFORMED BEFORE EACH FLIGHT
ACCESS: 414BL
424BL
242200-01-1
210 AC MAIN GENERATION
EL
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF AC GENERATION SIDE 1 AND SIDE 2
ISOLATION.
242400-01-2
210 AC EMERGENCY GENERATION
EL
OPC
MRB REFERENCE:
24.20.00/07
I:
75 FH
OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM.
CMR*
MRB 8
NOTE:
ETOPS RELEVANT
242400-01-3
242400-710-801
CMR REFERENCE:
242000-00001-1-C
MRB REFERENCE:
24.20.00/01
24.50.00/01
24.60.00/01
210 AC EMERGENCY GENERATION
EL
OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM.
OPC
I:
50 FH
CMP
CMR*
MRB 8
NOTE:
ETOPS RELEVANT
* * * * *
242200-710-801
242400-710-801
CMP REFERENCE:
24-2-0000-011
CMR REFERENCE:
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242400-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
242000-00001-1-C
MRB REFERENCE:
24.20.00/01
24.50.00/01
24.60.00/01
242400-01-4
210 AC EMERGENCY GENERATION
EL
OPC
I:
50 FH
OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM.
CMP
CMR*
MRB 8
NOTE:
ETOPS RELEVANT
242400-710-801
1
0.15 FAA
ETOPS
BETWEEN 60 AND 180
MIN D.T.
1
0.15 ALL
1
0.05 ALL
2
0.18 ALL
CMP REFERENCE:
24-2-0000-010
CMR REFERENCE:
242000-00001-1-C
MRB REFERENCE:
24.20.00/01
24.50.00/01
24.60.00/01
242400-02-2
210 AC EMERGENCY GENERATION
EL
OPC
I:
OPERATIONAL CHECK OF EMERGENCY GENERATOR MANUAL
CONNECTION.
24 MO
OR
4000 FH
CMR**
MRB 8
242400-710-802
CMR REFERENCE:
242000-00003-1-C
MRB REFERENCE:
24.20.00/11
R
242400-03-2
210 AC EMERGENCY GENERATION
EL
OPC
I:
48 MO
CMP
MRB 9
OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS.
242400-710-803
CMP REFERENCE:
24-2-0000-005
MRB REFERENCE:
24.20.00/08
242400-04-2
210 AC EMERGENCY GENERATION
EL
OPC
OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
I:
24 MO
OR
4000 FH
CMP
CMR**
MRB 8
242400-710-806
CMP REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
242400-04-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
CONNECTION.
24-2-0000-002
CMR REFERENCE:
242000-00004-1-C
MRB REFERENCE:
24.20.00/10
242400-05-2
210 AC EMERGENCY GENERATION
EL
OPC
I:
18 MO
MRB 8
OPERATIONAL CHECK OF CSM/G DISCONNECTION WITH
SIMULATED ENGINES FLAMED OUT CONDITION AND SLATS
EXTENDED.
242500-01-1
210 AC ESSENTIAL GENERATION SWITCHING
EL
242400-710-807
2
0.20 ALL
1
0.10 ALL
2
0.30 ALL
2
0.15 ALL
MRB REFERENCE:
24.20.00/12
OPC
I:
OPERATIONAL CHECK OF AC ESSENTIAL GENERATION MANUAL
AND AUTOMATIC SWITCHING.
24 MO
OR
12000 FH
CMR**
MRB 9
242500-710-801
CMR REFERENCE:
242000-00005-1-C
MRB REFERENCE:
24.20.00/09
242800-01-2
210 STATIC INVERTER AC GENERATION
EL
OPC
I:
650 FH
OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS
SUPPLY.
CMP
CMR*
MRB 8
242800-710-801
CMP REFERENCE:
24-2-0000-003
CMR REFERENCE:
242000-00002-1-C
MRB REFERENCE:
24.20.00/02
24.30.00/01
243500-01-1
210 DC MAIN GENERATION
EL
OPC
OPERATIONAL CHECK OF DC MAIN GENERATION SWITCHING.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
I:
24 MO
OR
12000 FH
CMR**
MRB 9
243200-710-801
CMR REFERENCE:
243000-00001-1-C
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
243500-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
MRB REFERENCE:
24.30.00/04
243500-02-1
210 DC ESSENTIAL & NORMAL GENERATION SWITCHING
EL
OPC
I:
OPERATIONAL CHECK OF DC ESSENTIAL GENERATION
SWITCHING.
24 MO
OR
12000 FH
CMR**
MRB 9
243400-710-801
2
0.10 ALL
1
0.10 ALL
1
0.15 ALL
*
0.01
1
0.15 ALL
*
0.01
1
0.15 ALL
*
0.25
CMR REFERENCE:
243000-00002-1-C
MRB REFERENCE:
24.30.00/05
R
243500-03-1
210 DC EMERGENCY GENERATION
EL
OPC
I:
1000 FH
MRB 8
OPERATIONAL CHECK OF DC BAT BUS AND DC ESS BUS
ISOLATION.
243851-01-1
120 BATTERY DC GENERATION
EL
243400-710-802
MRB REFERENCE:
24.30.00/06
RST
I:
12 MO
MRB 6
REMOVE BATTERIES 1 AND 2 FOR OVERHAUL.
243851-280-801
MRB REFERENCE:
24.30.00/03
ACCESS: 132AZ
243851-02-1
120 BATTERY DC GENERATION
EL
FNC
I:
REMOVE BATTERIES 1 AND 2 FOR CHECK IN WORKSHOP.
CE
NOTE
MRB 6
243851-280-802
MRB REFERENCE:
24.30.00/07
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
ACCESS: 132AZ
243852-01-2
160 BATTERY DC GENERATION
EL
RST
I:
12 MO
CMP
MRB 6
REMOVE BATTERY 3 (APU) FOR OVERHAUL.
ACCESS: 162KW
* * * * *
243852-280-801
CMP REFERENCE:
24-2-0000-007
162RW
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
243852-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
MRB REFERENCE:
24.30.00/03
243852-02-2
160 BATTERY DC GENERATION
EL
FNC
I:
CE
NOTE
MRB 6
REMOVE BATTERY 3 (APU) FOR CHECK IN WORKSHOP.
243852-280-801
1
0.15 ALL
*
0.25
1
1
0.15 ALL
0.15
1
0.10 ALL
1
0.10 ALL
1
0.15 ALL
MRB REFERENCE:
24.30.00/07
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
ACCESS: 162KW
245000-01-1
245000-02-1
162RW
200 AC MAIN DISTRIBUTION
EL
210
OPERATIONAL CHECK OF COMMERCIAL LOAD SHEDDING.
OPC
210 AC ESSENTIAL DISTRIBUTION
OPC
EL
I:
24 MO
MRB 9
MRB REFERENCE:
24.50.00/02
I:
24 MO
MRB 8
OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION.
245000-03-1
210 AC ESSENTIAL DISTRIBUTION
EL
210 AC ESSENTIAL DISTRIBUTION
AV
OPERATIONAL CHECK OF LEFT AND RIGHT FUEL PUMP 2
SHEDDING IN LAND RECOVERY CONFIGURATION.
245200-710-802
MRB REFERENCE:
24.50.00/03
24.60.00/02
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN
EMERGENCY CONFIGURATION.
245000-04-1
245100-710-801
245200-710-801
MRB REFERENCE:
24.50.00/04
OPC
I:
24 MO
OR
8000 FH
CMR**
MRB 8
282100-710-809
CMR REFERENCE:
245000-00001-1-C
MRB REFERENCE:
24.50.00/05
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
REV. DATE: JUL 01/21
SECTION:
2 -24
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
245000-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AC ESSENTIAL DISTRIBUTION
AV
OPC
I:
24 MO
SOURCE
MRB 8
OPERATIONAL CHECK AFT APU PUMP SHEDDING IN LAND
RECOVERY CONFIGURATION.
246000-03-1
200 DC ELECTRICAL LOAD DISTRIBUTION
EL
REFERENCE
282200-710-807
OPC
I:
24 MO
MRB 8
246000-710-801
MRB REFERENCE:
24.60.00/03
NOTE:
THIS TASK CAN BE PERFORMED AT THE SAME TIME AS TASK
245000-01-1.
E N D
SYSTEMS, APU AND POWER PLANT : ELECTRICAL POWER
M/H
APPLICABILITY
1
0.10 POST 44504
(28-3040)
POST 44603
(28-3041)
1
0.02 A330-200
POST 204137
(24-3049)
OR
A330-300
POST 204137
(24-3049)
OR
A330-200F
POST 204138
(24-3050)
OR
A330-800
POST 204137
(24-3049)
OR
A330-900
POST 204137
(24-3049)
MRB REFERENCE:
24.50.00/06
OPERATIONAL CHECK OF COMMERCIAL DC LOAD SHEDDING.
* * * * *
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-24
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
251100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 COCKPIT SEATS
AF
DET
I:
6 YE
SOURCE
MRB 8
DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT
ATTACHMENT.
251100-02-1
210 COCKPIT SEATS
AF
200 SEATS
AF
FNC
I:
24 MO
MRB 6,9
200 SEATS
CA
M/H
1
0.20 ALL
1
0.10 ALL
1
17.00 ALL
APPLICABILITY
DET
251100-200-804
MRB REFERENCE:
25.11.00/02
I: 24000 FH
MRB 8
DETAILED INSPECTION OF SEAT ATTACHMENTS, SEAT
STRUCTURE, SEAT BELTS AND BAGGAGE BAR.
252100-04-1
251100-200-801
MEN
MRB REFERENCE:
25.11.00/01
FUNCTIONAL CHECK OF HORIZONTAL/VERTICAL MECHANICAL
CONTROL CABLE ADJUSTMENT OF COCKPIT SEATS.
252100-01-1
REFERENCE
252100-210-801
MRB REFERENCE:
25.21.00/01
OPC
I:
CE
NOTE
MRB 8
OPERATIONAL CHECK OF AIRBAG SYSTEM BY DIAGNOSTIC TOOL
(V1.5&V23) OR EMA PTT PROCEDURE (NEXGEN).
252100-710-802
1
1.35 IF AMSAFE AIRBAG
SYSTEM INSTALLED
1
0.60 IF AMSAFE V1.5
OR
V23 AIRBAG SYSTEM
INSTALLED
1
2.93 IF AMSAFE AIRBAG
SYSTEM INSTALLED
MRB REFERENCE:
25.21.00/04
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
252100-05-1
200 SEATS
CA
DIS
I:
7 YE
NOTE
MRB 8
REMOVE EMA OF AIRBAG SYSTEM FOR IN SHOP DISCARD OF
BATTERY.
252158-920-801
MRB REFERENCE:
25.21.00/05
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
252100-06-1
200 SEATS
CA
DIS
I:
10 YE
NOTE
MRB 7,8
DISCARD AIRBAG INFLATOR ASSEMBLY/ASSEMBLIES.
MRB REFERENCE:
25.21.00/06
NOTE:
INTERVAL:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
252158-920-802
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
252100-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
252100-07-1
200 PASSENGER COMPARTMENT SEATS
AF
DET
I:
DETAILED INSPECTION OF AIRBAG SYSTEM COMPONENTS.
CE
NOTE
MRB 8
10 YE
NOTE
MRB 8
252100-710-808
1
1.50 IF AMSAFE AIRBAG
SYSTEM INSTALLED
1
2.93 IF AMSAFE NEXGEN
AIRBAG SYSTEM
INSTALLED
MRB REFERENCE:
25.21.00/07
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
252100-08-1
200 PASSENGER COMPARTMENT SEATS
AF
DIS
I:
DISCARD EMA OF AIRBAG SYSTEM.
252158-920-803
MRB REFERENCE:
25.21.00/08
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
PREP.: CABIN;
N
252100-09-1
220 PASSENGER COMPARTMENT SEATS
AF
OPC
I:
12 MO
MRB 8
OPERATIONAL CHECK OF PHARS BY MCSU DIAGNOSTIC TEST.
N
252100-10-1
220 PASSENGER COMPARTMENT SEATS
AF
DIS
252100-710-812
*
TBD
1
TBD IF SCHROTH PHARS
INSTALLED
1
TBD IF SCHROTH PHARS
INSTALLED
1
TBD IF THOMPSON AERO
SEATS WITH ILD
INSTALLED
MRB REFERENCE:
25.21.00/09
I:
DISCARD PHARS ASSEMBLY/ASSEMBLIES.
10 YE
NOTE
MRB 8
3 YE
MRB 9
252100-710-812
MRB REFERENCE:
25.21.00/10
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
N
252100-11-1
200 PASSENGER COMPARTMENT SEATS
AF
OPC
I:
OPERATIONAL CHECK OF INERTIA LOCKING DEVICE
MECHANISM.
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
252100-710-813
MRB REFERENCE:
25.21.00/11
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
252200-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CABIN ATTENDANT SEATS
AF
DET
I: 24000 FH
SOURCE
MRB 8
DETAILED INSPECTION OF CABIN ATTENDANT SEAT
ATTACHMENTS, SEAT STRUCTURE AND SEAT BELT (INCLUDING
SEAT BELT ATTACHMENTS AND BUCKLES).
252200-03-1
200 CABIN ATTENDANT SEATS
AF
OPC
252344-01-1
200 LININGS AND FURNISHINGS (DADO PANELS)
AF
OPC
I: 24000 FH
MRB 8
252344-02-1
200 LININGS AND FURNISHINGS (DADO PANELS)
AF
I:
4 C
MRB 9
252344-03-1
200 LININGS AND FURNISHINGS (DADO PANELS)
AF
VCK
I:
24 MO
MRB 8
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
1
0.20 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
OR
A330-200F
IF CAS INSTALLED
1
0.80 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
OPC
256800-210-802
1
0.15 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
25.23.44/01
I:
1000 FH
MRB 8
DETAILED INSPECTION OF COURIER AREA DECOMPRESSION
* * * * *
256800-710-803
256800-220-803
MRB REFERENCE:
APPLICABILITY
1.47 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
OR
A330-200F
IF CAS INSTALLED
MRB REFERENCE:
25.23.44/02
VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS
IN CABIN ARE CLOSED.
N
252200-210-803
M/H
1
MRB REFERENCE:
25.22.00/03
OPERATIONAL CHECK OF CABIN DECOMPRESSION PANELS
OPENING.
R
252200-210-802
MEN
MRB REFERENCE:
25.22.00/01
OPERATIONAL CHECK OF SEAT BELTS (INCLUDING HARNESS
ROLL-UP MECHANISM).
R
REFERENCE
1
TBD A330-200F
POST 58673
(25-3625)
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
252344-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
253000-01-1
MEN
M/H
APPLICABILITY
* * * * *
PANELS.
R
REFERENCE
25.23.44/03
200 BUFFET AND GALLEY
AF
DIS
I:
DISCARD GALLEY AIR EXTRACTION FILTER ELEMENT.
1400 FH
NOTE
MRB 9
72 MO
MRB 9
253000-920-802
2
5.60 ALL
1
4.13 ALL
1
0.30 IF AIR CHILLER
SYSTEM INSTALLED
*
0.02
1
0.30 AIR CHILLER SYSTEM
AND GALLEY WITH
GRILLES INSTALLED
MRB REFERENCE:
25.30.00/01
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
253000-03-1
200 BUFFET AND GALLEY
AF
DET
I:
DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT
POINTS.
253400-01-1
100 GALLEY COOLING
AF
253000-210-802
MRB REFERENCE:
25.30.00/03
RST
I:
1400 FH
NOTE
MRB 7
CLEAN AIR CHILLER CONDENSER AIR FILTER.
253400-160-801
MRB REFERENCE:
25.34.00/01
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 162ZW
253400-04-1
200 GALLEY COOLING
CA
RST
I:
1400 FH
NOTE
MRB 7
CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES
IN THE GALLEY CABINET.
253400-160-806
MRB REFERENCE:
25.34.00/04
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
253400-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
254000-01-1
200 LAVATORIES
CA
OPC
I: 12000 FH
MRB 9
OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP.
254000-02-1
200 LAVATORIES
CA
200 LAVATORIES
DET
I: 12000 FH
MRB 9
CA
150 LOWER DECK LAVATORIES
DET
I:
72 MO
MRB 9
AF
RST
I:
24 MO
MRB 9
255100-01-1
150 LOWER DECK LAVATORIES
AF
130 LOWER DECK CARGO LOADING SYSTEM
150
OPERATIONAL CHECK OF POWER DRIVE UNITS.
254000-210-804
257700-210-801
VCK
I:
1000 FH
MRB 8
AF
256800-210-801
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
0.30 ALL
1
1.93 ALL
1
0.30 POST 46203
1
0.20 POST 46203
1
1
0.15 A330-200
0.15 PRE 55381
OR
A330-300
PRE 55380
OR
A330-300
POST 55380
MRB REFERENCE:
25.47.00/02
OPC
I:
24 MO
MRB 9
255100-710-803
MRB REFERENCE:
25.51.00/01
NOTE:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
* * * * *
1
MRB REFERENCE:
25.47.00/01
VISUAL CHECK OF LDL RAPID DECOMPRESSION PANELS.
R
254000-220-801
MRB REFERENCE:
25.40.00/03
CLEANING OF DRAIN OPENINGS.
254700-03-1
0.10 ALL
MRB REFERENCE:
25.40.00/01
DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT
POINTS.
254700-01-1
1
MRB REFERENCE:
25.40.00/02
DETAILED INSPECTION OF WASTE COMPARTMENT FOR FIRE
CONTAINMENT CAPABILITY.
254000-03-1
254000-710-802
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
130 LOWER DECK CARGO LOADING SYSTEM
150
REMOVE XZ-LATCHES FOR DETAILED INSPECTION.
AF
DET
I: 34000 FH
MRB 8
255100-210-801
0.10 POST 201542
0.10
1
1
3.00 A330-200
3.00 PRE 55381
OR
A330-300
0.10 PRE 55380
0.10 OR
A330-300
POST 55380
POST 201542
*
*
150 LOWER DECK CARGO LOADING SYSTEM
AF
DET
I: 34000 FH
MRB 8
1
0.25 A330-200
POST 40611
(25-3168),
(25-3363)
PREP.: LDMCR;
*
6.00
ACCESS: 822
*
0.10
1
1
0.20 A330-200
0.20 PRE 55381
OR
A330-300
PRE 55380
OR
A330-300
POST 55380
POST 201542
1
1
0.10 A330-200
0.10 PRE 55381
OR
A330-300
PRE 55380
OR
A330-300
REMOVE CREW REST ROOM CONTAINER LATCHES AT FR 53.7
FOR DETAILED INSPECTION.
255100-10-1
130 LOWER DECK CARGO LOADING SYSTEM
150
GENERAL VISUAL INSPECTION OF XZ-LATCHES.
AF
255100-210-802
MRB REFERENCE:
25.51.00/03
GVI
I:
3200 FH
MRB 8
255100-210-816
MRB REFERENCE:
25.51.00/10
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255100-19-1
APPLICABILITY
*
*
MRB REFERENCE:
25.51.00/02
ACCESS: 821
822
255100-03-2
M/H
* * * * *
ACCESS: 821
822
255100-02-1
MEN
130 LOWER DECK CARGO LOADING SYSTEM
150
OPERATIONAL CHECK OF BRAKING ROLLER.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
AF
OPC
I:
48 MO
MRB 9
255100-200-802
MRB REFERENCE:
25.51.00/19
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255100-19-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 55380
POST 201542
255100-20-1
255100-21-1
130 LOWER DECK CARGO LOADING SYSTEM
AF
OPC
150
OPERATIONAL CHECK OF CENTERLINE GUIDE SWIVEL NOSES.
I:
130 LOWER DECK CARGO LOADING SYSTEM
AF
FNC
150
FUNCTIONAL CHECK OF DOOR SILL ANTI-ROLL OUT DEVICE.
I:
72 MO
MRB 9
130 LOWER DECK CARGO LOADING SYSTEM
AF
GVI
150
GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES.
1000 FH
MRB 9
255100-720-801
MRB REFERENCE:
25.51.00/21
I:
1000 FH
MRB 8
255100-210-818
1
1
0.50 A330-200
0.50 PRE 55381
OR
A330-300
0.10 PRE 55380
0.10 OR
A330-300
POST 55380
POST 201542
*
*
1
1
*
*
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
OPC
150
OPERATIONAL CHECK OF SWIVEL NOSE AT XZ-LATCHES EG
(ENTRANCE GUIDE) AND SWIVEL NOSES AT OVERRIDEABLE
CENTER LATCHES.
I:
72 MO
MRB 9
255100-200-804
MRB REFERENCE:
25.51.01/01
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
* * * * *
0.10 A330-200
0.10 POST 49610
OR
A330-300
POST 50567
MRB REFERENCE:
25.51.00/04
ACCESS: 821
822
255101-01-1
1
1
MRB REFERENCE:
25.51.00/20
ACCESS: 821
822
255100-22-1
255100-200-803
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
1
1
0.10 A330-200
0.10 PRE 55381
OR
A330-300
0.10 PRE 55380
0.10 OR
A330-300
POST 55380
POST 201542
0.10 A330-200F
0.10 OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255101-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-900
255101-02-1
255101-03-1
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
150
REMOVE XZ-LATCHES FOR DETAILED INSPECTION.
AF
150 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
DET
I: 34000 FH
MRB 8
1
1
3.00 A330-200F
3.00 OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
1
0.25 A330-200
POST 56839
OR
A330-800
POST 56839
1
1
0.10 A330-200F
0.10 OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
1
1
0.50 A330-200F
0.50 OR
A330-200
POST 55381
MRB REFERENCE:
25.51.01/02
DET
I: 34000 FH
MRB 8
REMOVE LOWER DECK-MOBIL CREW REST CONTAINER LATCHES
FOR DETAILED INSPECTION.
255101-04-1
255100-210-813
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
150
OPERATIONAL CHECK OF BRAKING ROLLER AND SWIVEL
CASTER.
OPC
255100-210-814
MRB REFERENCE:
25.51.01/03
I:
48 MO
MRB 9
255100-200-805
MRB REFERENCE:
25.51.01/04
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255101-08-1
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
DET
150
DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR
WEAR AND DAMAGE.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
I:
24 MO
MRB 9
255100-210-811
MRB REFERENCE:
25.51.01/08
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255101-08-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
150
GENERAL VISUAL INSPECTION OF XZ LATCHES.
AF
GVI
I:
3200 FH
MRB 8
255100-210-810
MRB REFERENCE:
25.51.01/10
1
1
0.20 A330-200F
0.20 OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
1
1
0.25 A330-200
0.25 POST 55381
PRE 205271
OR
0.10 A330-300
0.10 POST 55380
PRE 201542
PRE 205272
OR
A330-200F
PRE 205271
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255101-16-1
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
FNC
150
FUNCTIONAL CHECK OF DOOR SILL ANTI-ROLL OUT DEVICE.
I:
1000 FH
MRB 9
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
GVI
150
GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES.
I:
1000 FH
MRB 8
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
255100-210-817
MRB REFERENCE:
25.51.01/05
ACCESS: 821
822
* * * * *
255100-720-802
MRB REFERENCE:
25.51.01/16
ACCESS: 821
822
255101-17-1
APPLICABILITY
* * * * *
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255101-10-1
M/H
*
*
1
1
*
*
0.10 A330-200
0.10 POST 55381
PRE 205271
OR
0.10 A330-300
0.10 POST 55380
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255101-17-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PRE 201542
PRE 205272
OR
A330-200F
PRE 205271
255101-18-1
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
GVI
150
GENERAL VISUAL INSPECTION OF DOOR SILL YZ- LATCH
PAWL, ANTI ROLL OUT DEVICE AND ACTUATION MECHANISM.
I:
750 FC
MRB 8
255100-210-819
MRB REFERENCE:
25.51.01/17
ACCESS: 821
822
255101-19-1
*
*
130 ADVANCED LOWER DECK CARGO LOADING SYSTEM
AF
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF BRAKING ROLLER IN DOOR SILL AREA
OF FWD CC.
255100-200-806
*
130 LOWER DECK FORWARD CARGO COMPARTMENT
AF
VCK
I:
10 DY
CMP
MRB 8
VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING
STRIPS, PROTECTION PLATES, CENTER LINE COVER PLATES,
ACCESS DOORS, DECOMPRESSION PANELS AND PRESSURE
EQUALIZATION VALVES.
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
255200-210-801
1
0.18 A330-200F
0.18 POST 205271
OR
A330-200
POST 205271
0.10 OR
0.10 A330-300
POST 205272
OR
A330-800
OR
A330-900
0.27 A330-200F
POST 205271
OR
A330-200
POST 205271
0.10 OR
A330-300
POST 205272
OR
A330-800
OR
A330-900
0.35 ALL
CMP REFERENCE:
25-2-0000-002
MRB REFERENCE:
25.52.00/01
25.52.00/02
NOTE:
* * * * *
1
MRB REFERENCE:
25.51.01/18
ACCESS: 821
255200-01-1
1
1
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255200-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
R
255200-03-1
130 LOWER DECK FORWARD CARGO COMPARTMENT
AF
VCK
I:
1000 FH
MRB 9
VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE
ROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OF
CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY
255200-210-802
1
1.00 ALL
1
0.40 A330-200
POST 45395
(25-3436),
(25-3643)
OR
A330-200
POST 56835
0.80 OR
A330-300
POST 43719
(25-3324)
OR
A330-300
POST 56834
(25-3699)
OR
A330-200F
OR
A330-300
POST 204139
(25-3520),
(25-3699)
OR
A330-900
POST 207250
MRB REFERENCE:
25.52.00/03
NOTE:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255200-04-1
130 LOWER DECK FORWARD CARGO COMPARTMENT
AF
OPC
REMOVE AIR STOP VALVE FOR IN SHOP OPERATIONAL CHECK.
I:
24 MO
OR
5000 FH
CMP
MRB 8
NOTE:
ETOPS RELEVANT
255200-200-803
CMP REFERENCE:
25-2-0000-001
MRB REFERENCE:
25.52.00/04
ACCESS: 131JG
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
*
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255200-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
130 LOWER DECK FORWARD CARGO COMPARTMENT
AF
VCK
I:
1000 FH
SOURCE
MRB 9
VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR
EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS
NECESSARY.
255300-01-1
150 LOWER DECK AFT CARGO COMPARTMENT
AF
VCK
I:
10 DY
CMP
MRB 8
AF
VCK
255300-210-801
M/H
APPLICABILITY
1
1.00 A330-200F
OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
1
0.30 ALL
1
1.00 ALL
1
0.40 A330-200
POST 45395
(25-3436),
(25-3643)
OR
A330-200
POST 56835
CMP REFERENCE:
25-2-0000-002
MRB REFERENCE:
25.52.00/01
25.52.00/02
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
150 LOWER DECK AFT CARGO COMPARTMENT
255200-210-803
MEN
MRB REFERENCE:
25.52.00/06
VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING
STRIPS, PROTECTION PLATES, CENTER LINE COVER PLATES
AND DECOMPRESSION PANELS.
255300-03-1
REFERENCE
I:
1000 FH
MRB 9
VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE
ROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OF
CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY.
255300-210-804
MRB REFERENCE:
25.52.00/03
NOTE:
PLANNING:
- CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE
REMOVED IF INSTALLED
255300-04-1
150 LOWER DECK AFT CARGO COMPARTMENT
AF
OPC
REMOVE AIR STOP VALVE FOR IN SHOP OPERATIONAL CHECK.
I:
24 MO
OR
5000 FH
CMP
MRB 8
NOTE:
ETOPS RELEVANT
* * * * *
255300-200-803
CMP REFERENCE:
25-2-0000-001
MRB REFERENCE:
25.52.00/04
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255300-04-1
ZONE
* * * * *
ACCESS: 151PG
255300-06-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
MEN
M/H
APPLICABILITY
* * * * *
151VK
150 LOWER DECK AFT CARGO COMPARTMENT
AF
VCK
I:
1000 FH
MRB 9
VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR
EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS
NECESSARY.
255400-01-1
REFERENCE
160 LOWER DECK BULK CARGO COMPARTMENT
AF
VCK
255300-210-805
*
0.88 OR
A330-300
POST 43719
(25-3324)
OR
A330-300
POST 56834
(25-3699)
OR
A330-200F
OR
A330-300
POST 204139
(25-3520),
(25-3699)
OR
A330-900
POST 207250
1
1.00 A330-200F
OR
A330-200
POST 55381
OR
A330-300
POST 55380
PRE 201542
OR
A330-800
OR
A330-900
1
0.25 ALL
MRB REFERENCE:
25.52.00/06
I:
10 DY
CMP
MRB 8
VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING
STRIPS, ACCESS DOOR AT C73, DECOMPRESSION PANELS AND
PRESSURE EQUALIZATION VALVE.
255400-210-801
CMP REFERENCE:
25-2-0000-002
MRB REFERENCE:
25.54.00/01
25.54.00/02
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255400-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
160 LOWER DECK BULK CARGO COMPARTMENT
AF
DET
I:
24 MO
SOURCE
MRB 9
DETAILED INSPECTION OF DIVIDER NETS, NET ATTACHMENT
POINTS, NET CONNECTING DEVICES AND TENSION BUCKLES.
255400-05-1
160 LOWER DECK BULK CARGO COMPARTMENT
AF
DET
160 LOWER DECK BULK CARGO COMPARTMENT
I:
24 MO
MRB 9
AF
230 MAIN DECK CARGO COMPARTMENT (INCLUDING
DRAINAGE AND BARRIER WALL)
DET
I:
230 MAIN DECK CARGO COMPARTMENT (INCLUDING
DRAINAGE AND BARRIER WALL)
24 MO
MRB 9
AF
DET
I:
AF
VCK
I:
3 MO
OR
1000 FH
MRB 8
250 MAIN DECK CARGO COMPARTMENT (INCLUDING
DRAINAGE AND BARRIER
1000 FH
MRB 9
255400-210-805
255400-210-806
AF
GVI
532100-220-833
255800-210-801
I:
1000 FH
MRB 8
255500-200-804
AF
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF BRAKING ROLLER.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
1
0.30 ALL
1
0.20 ALL
1
0.30 A330-200F
1
0.50 A330-200F
1
0.02 A330-200F
*
0.02
1
0.10 A330-200F
MRB REFERENCE:
25.55.00/06
ACCESS: 835
200 MAIN DECK CARGO LOADING SYSTEM
0.50 ALL
MRB REFERENCE:
25.55.00/05
GENERAL VISUAL INSPECTION OF MD WINDOW PROTECTION
COVER.
255600-01-1
1
MRB REFERENCE:
25.55.00/01
VISUAL CHECK OF THE DRAIN FUNNELS WITHIN THE DRAIN
PANS FOR CLOGGING OR OBSTRUCTION AND CLEAN AS
NECESSARY.
255500-06-1
APPLICABILITY
MRB REFERENCE:
25.54.00/06
DETAILED INSPECTION OF BARRIER WALL, DECOMPRESSION
PANEL, SMOKE CURTAIN AND ACCESS DOOR SEALING.
255500-05-1
M/H
MRB REFERENCE:
25.54.00/05
DETAILED INSPECTION OF SCREEN DECOMPRESSION
TARPAULINS.
255500-01-1
255400-210-804
MEN
MRB REFERENCE:
25.54.00/04
DETAILED INSPECTION OF NET SCREENS, NET SCREEN
ATTACHMENT POINTS AND TENSION BUCKLES.
255400-06-1
REFERENCE
255600-200-804
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
255600-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
25.56.00/01
255600-02-1
200 MAIN DECK CARGO LOADING SYSTEM
AF
GVI
I:
3200 FH
MRB 8
GENERAL VISUAL INSPECTION OF XZ-LATCHES.
255600-03-1
200 MAIN DECK CARGO LOADING SYSTEM
AF
230 MAIN DECK CARGO LOADING SYSTEM
DET
I: 34000 FH
MRB 8
AF
200 MAIN DECK CARGO LOADING SYSTEM
OPC
I:
72 MO
MRB 9
AF
200 MAIN DECK CARGO LOADING SYSTEM
GVI
I:
3200 FH
MRB 8
AF
200 MAIN DECK CARGO LOADING SYSTEM
DET
I: 34000 FH
MRB 8
AF
OPC
211 COCKPIT ESCAPE FACILITIES
AF
DET
212
DETAILED INSPECTION OF EMERGENCY ESCAPE ROPE AND ROPE
ATTACHMENT.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
4.00 A330-200F
255600-200-802
1
0.10 A330-200F
POST 58552
255600-210-803
1
0.15 A330-200F
POST 58959
255600-220-801
1
2.00 A330-200F
POST 58959
1
0.15 A330-200F
POST 58959
1
1
0.20 ALL
0.20
MRB REFERENCE:
25.56.00/14
I:
72 MO
MRB 8
OPERATIONAL CHECK OF 16/20 FT YZ-LATCH SWIVEL NOSES.
256141-01-1
1
MRB REFERENCE:
25.56.00/13
REMOVE 16/20 FT YZ-LATCHES FOR DETAILED INSPECTION.
255600-15-1
255600-210-802
MRB REFERENCE:
25.56.00/04
GENERAL VISUAL INSPECTION OF 16/20 FT YZ-LATCHES.
255600-14-1
0.30 A330-200F
MRB REFERENCE:
25.56.00/03
OPERATIONAL CHECK OF XZ-ENDSTOP SWIVEL NOSES.
255600-13-1
1
MRB REFERENCE:
25.56.00/02
REMOVE XZ-LATCHES FOR DETAILED INSPECTION.
255600-04-1
255600-210-801
255600-200-801
MRB REFERENCE:
25.56.00/15
I:
6 YE
MRB 8
256141-200-801
MRB REFERENCE:
25.61.00/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
256141-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
256200-08-1
M/H
*
*
0.01
0.01
APPLICABILITY
* * * * *
ACCESS: 211HC
212HC
R
MEN
200 CABIN ESCAPE FACILITIES
AF
DIS
I:
CE
NOTE
MRB 8
REMOVE ESCAPE SLIDE FOR DISCARD OF INFLATABLE SLIDE
ASSEMBLY.
256241-920-801
1
TBD ALL
2
2
2
2
2
2
2
2
2.00 ALL
2.00
2.00
2.00
2.00
2.00
2.00
2.00
2
1.20 ALL
*
2.80
MRB REFERENCE:
25.62.00/08
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
D
256241-01-1
R
256241-02-1
256241-03-1
************** TASK DELETED **************
831
832
833
834
841
842
843
844
CABIN ESCAPE FACILITIES
AF
RST
REMOVE ESCAPE SLIDE/RAFT FOR IN SHOP OVERHAUL.
I:
CE
NOTE
MRB 6,8
MRB REFERENCE:
25.62.00/02
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
200 CABIN ESCAPE FACILITIES
AF
OPC
I:
36 MO
NOTE 10
MRB -
OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT.
256532-02-1
256200-710-801
MRB REFERENCE:
25.62.00/03
PREP.: SLIDE/RAFT TEST PREPARATION;
SLIDE/RAFT;
D
256200-280-801
************** TASK DELETED **************
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
256532-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 EMERGENCY LOCATOR TRANSMITTER-PORTABLE
CA
RST
I:
CE
NOTE
SOURCE
MRB 9
REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER FOR IN
SHOP BATTERY REPLACEMENT AND OPERATIONAL CHECK OF:
- WATER SWITCH
- GPS FUNCTIONALITY
- 406 MHZ DISTRESS SIGNAL TRANSMISSION.
REFERENCE
256532-920-802
MEN
1
MRB REFERENCE:
25.65.32/03
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 831
N
256532-04-1
841
200 EMERGENCY LOCATOR TRANSMITTER-PORTABLE
*
CA
OPC
I:
60 MO
NOTE
MRB 9
OPERATIONAL CHECK OF SURVIVAL EMERGENCY LOCATOR
TRANSMITTER (ELT(S)).
256532-710-801
1
M/H
APPLICABILITY
0.10 IF SURVIVAL ELT
FROM HONEYWELL
07217 INSTALLED
OR
IF SURVIVAL ELT
FROM THALES FAU27
INSTALLED
OR
IF SURVIVAL ELT
FROM ELTA FORMER
CEIS 649E2
INSTALLED
OR
IF SURVIVAL ELT
0.04 FROM ELTA F6614
INSTALLED
TBD ALL
MRB REFERENCE:
25.65.32/04
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 831
N
256532-05-1
841
200 EMERGENCY LOCATOR TRANSMITTER-PORTABLE
*
CA
DIS
I:
CE
NOTE
MRB 9
DISCARD BATTERY OF SURVIVAL EMERGENCY LOCATOR
TRANSMITTER (ELT(S)).
256532-920-803
1
MRB REFERENCE:
25.65.32/05
0.04
TBD IF SURVIVAL ELT
FROM TECHTEST U2615
INSTALLED
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 831
841
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
*
REV. DATE: JUL 01/21
SECTION:
2-25
0.04
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
256534-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 EMERGENCY VHF TRANSCEIVER
CA
FNC
I:
24 MO
SOURCE
MRB 9
REMOVE EMERGENCY VHF TRANSCEIVER FOR SHOP INSPECTION.
R
256535-01-1
210 EMERGENCY LOCATOR TRANSMITTER SYSTEM
RA
OPC
256535-03-1
200 EMERGENCY LOCATOR TRANSMITTER SYSTEM
256534-000-801
MEN
I:
24 MO
MRB 8
256500-710-803
M/H
APPLICABILITY
1
0.30 IF EMERGENCY VHF
TRANSCEIVER
INSTALLED
1
0.05 PRE
208191
1
0.50 PRE
208191
*
0.04
1
0.50 PRE
*
0.04
MRB REFERENCE:
25.65.34/01
OPERATIONAL CHECK OF AUTOMATIC FIXED EMERGENCY
LOCATOR TRANSMITTER (ELT(AF)) SYSTEM BY MANUAL
ACTIVATION.
R
REFERENCE
MRB REFERENCE:
25.65.35/01
CA
DIS
I:
CE
NOTE
MRB 8
REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER
(ELT(AF)) FOR IN SHOP DISCARD OF BATTERIES.
256500-720-806
MRB REFERENCE:
25.65.35/03
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 831
R
256535-04-1
841
200 EMERGENCY LOCATOR TRANSMITTER SYSTEM
CA
OPC
I:
72 MO
MRB 8
REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER
(ELT(AF)) FOR IN SHOP OPERATIONAL CHECK OF ELT(AF).
ACCESS: 831
N
256535-05-1
841
260 EMERGENCY LOCATOR TRANSMITTER SYSTEM
CA
GVI
150 BEACON - LOW FREQUENCY UNDERWATER LOCATOR
AV
OPC
170
OPERATIONAL CHECK OF LOW FREQUENCY UNDERWATER LOCATOR
BEACON.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
208191
MRB REFERENCE:
25.65.35/04
I:
36 MO
MRB 8
GENERAL VISUAL INSPECTION OF EXTERNAL ELT ANTENNA.
256536-01-1
256500-720-807
256500-210-802
1
TBD ALL
MRB REFERENCE:
25.65.35/05
I:
36 MO
MRB 9
256500-710-805
MRB REFERENCE:
25.65.36/01
1
1
0.13 POST 207095
0.13 (25-3676),
(25-3718),
(25-3728)
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
256536-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
M/H
APPLICABILITY
*
0.10
1
1
0.05 POST 207095
0.05 (25-3676),
(25-3718),
(25-3728)
*
0.10
1
0.12 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
OR
A330-200F
IF MEGAPHONE
INSTALLED
1
0.05 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
OR
A330-200F
IF MEGAPHONE
INSTALLED
* * * * *
ACCESS: 822
256536-02-1
MEN
150 BEACON - LOW FREQUENCY UNDERWATER LOCATOR
AV
DIS
170
REMOVE LOW FREQUENCY UNDERWATER LOCATOR BEACON FOR IN
SHOP DISCARD OF BATTERY.
I:
72 MO
NOTE
MRB 9
256500-920-801
MRB REFERENCE:
25.65.36/02
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 822
256551-01-1
200 MEGAPHONE
CA
DIS
I:
12 MO
MRB 9
DISCARD MEGAPHONE BATTERIES.
256551-02-1
200 MEGAPHONE
MRB REFERENCE:
25.65.51/01
CA
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF MEGAPHONE.
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
256551-920-801
256551-710-801
MRB REFERENCE:
25.65.51/02
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 19
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
256652-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 LIFE VESTS
CA
RST
I:
CE
NOTE
SOURCE
MRB 9
REMOVE LIFE VESTS FOR IN SHOP OVERHAUL.
200 CREW REST ROOM (CABIN)
CA
DET
I: 36000 FH
MRB 8
DETAILED INSPECTION OF SEAT BELTS, BELT ATTACHMENTS
AND LOWER BUNK STRUCTURE.
257500-01-1
257500-02-1
I:
150 CREW REST ROOM (UNDERFLOOR)
I:36000 CRR FH
DET
24 MO
MRB 8
150 CREW REST ROOM (UNDERFLOOR)
AF
DET
MRB 8
257400-210-801
257500-710-801
257500-220-801
I:
6 YE
MRB 8
257500-210-802
AF
OPC
I:48CRR MO
MRB 9
OPERATIONAL CHECK OF DOOR HINGE AND LOCK.
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
2.75 ALL
1
0.15 IF FCRC INSTALLED
1
1
0.10 IF LDMCR INSTALLED
0.10
1
0.15 IF LDMCR INSTALLED
1
1.00 IF LDMCR INSTALLED
*
6.00
1
0.05 IF LDMCR AND LDL
INSTALLED
MRB REFERENCE:
25.75.00/04
PREP.: LDMCR;
150 CREW REST ROOM (UNDERFLOOR)
1
MRB REFERENCE:
25.75.00/02
DETAILED INSPECTION OF CARGO COMPARTMENT CEILING
WELL, INTERFACE LININGS AND OF THE OUTSIDE OF THE
CONTAINER.
257500-05-1
APPLICABILITY
MRB REFERENCE:
25.75.00/01
DETAILED INSPECTION OF BED BELTS AND BELT ATTACHMENTS
ON CREW REST BUNKS.
257500-04-1
M/H
MRB REFERENCE:
25.74.00/01
150 CREW REST ROOM (UNDERFLOOR)
AF
OPC
260
OPERATIONAL CHECK OF EMERGENCY EXIT HATCH OPENING
FROM INSIDE AND FROM OUTSIDE.
AF
256652-920-801
MEN
MRB REFERENCE:
25.66.52/01
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
257400-01-1
REFERENCE
257500-710-803
MRB REFERENCE:
25.75.00/06
REV. DATE: JUL 01/21
SECTION:
2 -25
PAGE 20
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
257500-13-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
150 CREW REST ROOM (UNDERFLOOR)
AF
GVI
I:
48 MO
SOURCE
MRB 8
GENERAL VISUAL INSPECTION OF HATCH SEALS, DOOR SEALS
AND BELLOW SEALS.
REFERENCE
257500-210-808
E N D
M/H
APPLICABILITY
1
0.15 IF LDMCR INSTALLED
*
6.00
MRB REFERENCE:
25.75.00/13
PREP.: LDMCR;
* * * * *
MEN
* * * * *
SYSTEMS, APU AND POWER PLANT : EQUIPMENT/FURNISHINGS
REV. DATE: JUL 01/21
SECTION:
2-25
PAGE 21
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
261100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 MAIN LANDING GEAR BAY FIRE AND OVERHEAT
DETECTION
AV
OPC
I:
2000 FH
SOURCE
MRB 8
130 AVIONICS COMPARTMENT SMOKE DETECTION
AV
RST
I:
42 MO
MRB 8
REMOVE AVIONICS SMOKE DETECTION PICCOLO TUBES FOR
CLEANING.
ACCESS: 131EF
261600-01-1
261100-740-801
261500-100-801
1
M/H
APPLICABILITY
TBD POST 207753
POST 207754
AV
1
1.50 ALL
*
0.40
1
0.20 ALL
1
1
0.05 IF LDMCR INSTALLED
0.05
1
0.60 IF LDMCR INSTALLED
MRB REFERENCE:
26.15.00/02
132EF
210 LOWER DECK CARGO COMPT AND AVIONIC
COMPARTMENT
MEN
MRB REFERENCE:
26.11.00/01
BITE TEST OF THE FDU THROUGH MCDU.
261500-02-1
REFERENCE
OPC
I:
6000 FH
NOTE
MRB 9
261600-710-803
MRB REFERENCE:
26.15.00/01
26.16.00/01
OPERATIONAL CHECK OF LOWER DECK CARGO COMPARTMENT AND
AVIONICS COMPARTMENT SMOKE DETECTION BY PTT.
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
261800-01-1
100 AUXILIARY AREAS SMOKE DETECTION
AV
OPC
210
OPERATIONAL CHECK OF LDMCR SMOKE DETECTION BY PTT.
I:
4000 FH
NOTE
MRB 9
261800-710-801
MRB REFERENCE:
26.18.00/01
NOTE:
PLANNING:
- TASK IS INCLUDED IN MANUFACTURER'S CREW REST ROOM
(UNDERFLOOR) REMOVAL/INSTALLATION PROCEDURE. CREDIT
CAN BE TAKEN FOR PERFORMANCE OF THIS TASK AT THIS
OPPORTUNITY
261800-02-1
150 AUXILIARY AREAS SMOKE DETECTION
AF
RST
I:72CRR MO
MRB 6
REMOVE AND CLEAN LDMCR SMOKE DETECTORS.
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
261800-100-801
MRB REFERENCE:
26.18.00/02
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
261800-03-1
261800-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 AUXILIARY AREAS SMOKE DETECTION
AV
OPC
210
OPERATIONAL CHECK OF LDMCR STAIRHOUSE SMOKE DETECTION
SYSTEM BY MCDU.
I:
210 AUXILIARY AREA SMOKE DETECTION
I:
AV
OPC
24 MO
SOURCE
MRB 9
100 AUXILIARY AREAS SMOKE DETECTION
AV
OPC
24 MO
MRB 9
210 AUXILIARY AREAS SMOKE DETECTION
AV
I:24CRR MO
MRB 9
231 AUXILIARY AREAS SMOKE DETECTION
AF
OPC
I:
24 MO
MRB 8
RST
I: 20000 FH
MRB 7
210 AUXILIARY AREAS SMOKE DETECTION
AV
134 AUXILIARY AREAS SMOKE DETECTION
OPC
I:
24 MO
MRB 8
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
1
0.10 IF FCRC INSTALLED
261800-750-801
1
0.40 IF LDMCR INSTALLED
261800-710-811
1
0.20 IF SMOKE DETECTORS
WITH FIN 5WB/6WB
INSTALLED
OR
IF SMOKE DETECTORS
WITH FIN 7WB/8WB
INSTALLED
261800-100-806
1
1.00 IF DUCTED
DETECTORS
5WB / 6WB
OR
IF DUCTED
DETECTORS
7WB / 8WB
AF
RST
261800-710-810
I: 20000 FH
MRB 7
261800-100-807
MRB REFERENCE:
SMOKE
WITH FIN
INSTALLED
SMOKE
WITH FIN
INSTALLED
1
3.20 IF SMOKE DETECTORS
WITH FIN 3WB / 4WB
INSTALLED AND
ACTIVATED
1
0.40 IF SMOKE DETECTORS
WITH FIN 3WB / 4WB
INSTALLED AND
MRB REFERENCE:
26.18.00/12
REMOVE IFEC PICCOLO TUBES FOR CLEANING.
* * * * *
0.10 IF LDMCR STAIRHOUSE
0.10 SMOKE DETECTION
SYSTEM INSTALLED
MRB REFERENCE:
26.18.00/11
OPERATIONAL CHECK OF IFEC SMOKE DETECTION BY MCDU.
261800-13-1
1
1
MRB REFERENCE:
26.18.00/10
REMOVE VCC TUBES FOR CLEANING.
261800-12-1
APPLICABILITY
MRB REFERENCE:
26.18.00/06
OPERATIONAL CHECK OF VCC SMOKE DETECTION BY MCDU.
261800-11-1
261800-710-804
M/H
MRB REFERENCE:
26.18.00/04
OPERATIONAL CHECK OF LDMCR SMOKE DETECTORS WITH
AEROSOL.
261800-10-1
261800-710-803
MEN
MRB REFERENCE:
26.18.00/03
OPERATIONAL CHECK OF FCRC SMOKE DETECTION SYSTEM BY
MCDU.
261800-05-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
261800-13-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
0.30
1
0.10 IF SMOKE DETECTORS
WITH FIN 31WB/FIN
32WB INSTALLED AND
ACTIVATED
1
0.20 IF SMOKE DETECTORS
WITH FIN 31WB/FIN
32WB INSTALLED AND
ACTIVATED
1
0.20 IF SMOKE DETECTORS
WITH FIN 35WB / FIN
36WB INSTALLED AND
ACTIVATED
1
0.20 IF SMOKE DETECTORS
WITH FIN 35WB / FIN
36WB INSTALLED AND
ACTIVATED
1
0.10 IF CCRM INSTALLED
*
0.02
1
1.00 POST 46441
POST 46755
(26-3020)
*
0.20
* * * * *
26.18.00/13
ACTIVATED
ACCESS: 132EG
261800-18-1
210 AUXILIARY AREAS SMOKE DETECTION
AV
OPC
I:
18 MO
MRB 9
OPERATIONAL CHECK OF FCC SMOKE DETECTION BY MCDU.
261800-19-1
130 AUXILIARY AREAS SMOKE DETECTION
AV
210 AUXILIARY AREAS SMOKE DETECTION
AV
RST
I: 18000 FH
MRB 8
120 AUXILIARY AREAS SMOKE DETECTION
AV
OPC
I:
24 MO
MRB 9
210 AUXILIARY AREAS SMOKE DETECTION
AV
261800-710-816
MRB REFERENCE:
26.18.00/20
RST
I: 17000 FH
MRB 8
REMOVE AND CLEAN PICCOLO TUBES OF ALNA V2 CENTER RACK
IV SMOKE DETECTION.
261800-23-1
261800-100-810
MRB REFERENCE:
26.18.00/19
OPERATIONAL CHECK OF ALNA V2 CENTER RACK IV SMOKE
DETECTION BY MCDU.
261800-21-1
261800-710-817
MRB REFERENCE:
26.18.00/18
REMOVE AND CLEAN PICCOLO TUBES OF FCC RACK SMOKE
DETECTION.
261800-20-1
OPC
261800-100-809
MRB REFERENCE:
26.18.00/21
I:
18 MO
MRB 9
OPERATIONAL CHECK OF CCRM SMOKE DETECTION SYSTEM BY
MCDU.
261800-710-821
MRB REFERENCE:
26.18.00/23
ACCESS: 831
261801-01-1
153 BULK AVIONICS COMPARTMENT SMOKE DETECTION
(MOD 46441)
AF
RST
I:
36 MO
MRB 8
261800-100-802
MRB REFERENCE:
26.18.01/01
REMOVE AND CLEAN BULK AVIONICS SMOKE DETECTOR PICCOLO
TUBES.
ACCESS: 151TF
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
APPLICABILITY
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
261801-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 BULK AVIONICS COMPARTMENT SMOKE DETECTION
(MOD 46441)
AV
OPC
I:
18 MO
SOURCE
MRB 9
210 MAIN DECK CARGO COMPARTMENT SMOKE DETECTION
AV
OPC
I:
3200 FH
MRB 9
OPERATIONAL CHECK OF MAIN DECK CARGO COMPARTMENT
SMOKE DETECTION BY PTT.
261900-02-1
210 MAIN DECK CARGO COMPARTMENT SMOKE DETECTION
AV
210 ENGINE FIRE EXTINGUISHING
AV
261900-710-802
M/H
APPLICABILITY
1
0.20 POST 46441
POST 46755
(26-3020)
1
0.20 A330-200F
1
0.20 A330-200F
1
0.05 ALL
2
2
0.50 ALL
0.50
*
*
0.10
0.10
1
1
0.10 ALL
0.10
MRB REFERENCE:
26.19.00/01
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF MDCC
ISOLATION VALVES.
262100-04-1
261800-710-807
MEN
MRB REFERENCE:
26.18.01/02
OPERATIONAL CHECK OF THE BULK AVIONICS COMPARTMENT
SMOKE DETECTION SYSTEM VIA MCDU.
261900-01-1
REFERENCE
OPC
261900-710-803
MRB REFERENCE:
26.19.00/02
I:
OPERATIONAL CHECK OF FIRE EXTINGUISHING SYSTEM.
2000 FH
NOTE
MRB 9
120 MO
NOTE
MRB 6,9
261200-710-812
MRB REFERENCE:
26.21.00/01
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
262100-10-1
450 ENGINE FIRE EXTINGUISHING
AV
460
REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF
PRESSURE SWITCH SETTING.
FNC
I:
262141-200-805
MRB REFERENCE:
26.21.00/04
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 453CL
463CL
262100-11-1
453CR
463CR
210 ENGINE FIRE EXTINGUISHING
450
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
AF
OPC
I:
24 MO
MRB 9
262100-710-809
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262100-11-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
262100-12-1
262100-13-1
262100-14-1
417AL
427AL
418AR
428AR
453CL
463CL
0.10
*
*
0.10
0.10
I: 12000 FH
MRB 8
2
2
2.00 ALL
2.00
*
*
0.30
0.30
1
1
1
0.15 ALL
0.15
0.15
*
*
0.10
0.10
1
1
1
0.30 ALL
0.30
0.30
MRB REFERENCE:
24.20.00/15
26.21.00/03
28.24.00/02
*
*
0.10
0.10
262141-920-803
2
2
0.50 ALL
0.50
*
*
0.10
0.10
262100-720-819
MRB REFERENCE:
26.21.00/08
FNC
I:
48 MO
MRB 9
262100-710-810
MRB REFERENCE:
26.21.00/07
453CR
463CR
OPC
I:
24 MO
CMP
MRB 8
AF
262100-710-811
CMP REFERENCE:
24-2-0000-006
453CR
463CR
450 ENGINE FIRE EXTINGUISHING
460
DISCARD CARTRIDGE.
ACCESS: 453CL
463CL
1
MRB REFERENCE:
26.21.00/02
453CR
463CR
210 ENGINE FIRE EXTINGUISHING
AV
450
460 OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW
FUNCTION.
ACCESS: 453CL
463CL
262100-15-1
416AR
426AR
210 ENGINE FIRE EXTINGUISHING
AV
450
460 FUNCTIONAL CHECK OF FIRING CIRCUIT CONTINUITY.
ACCESS: 453CL
463CL
M/H
453CR
463CR
410 ENGINE FIRE EXTINGUISHING
AF
FNC
420
FUNCTIONAL CHECK OF DISTRIBUTION PIPING FOR LEAKAGE
AND OBSTRUCTION.
ACCESS: 415AL
425AL
MEN
DIS
I:
120 MO
MRB 9
MRB REFERENCE:
26.21.00/09
453CR
463CR
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
APPLICABILITY
* * * * *
460 OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER BOTTLE
LOW PRESSURE INDICATING CIRCUIT.
ACCESS: 453CL
463CL
REFERENCE
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262200-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 APU FIRE EXTINGUISHING
AV
OPC
I:
3000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM.
R
262200-01-3
210 APU FIRE EXTINGUISHING
AV
OPC
REFERENCE
262200-710-801
MEN
M/H
APPLICABILITY
1
0.20 NON-ETOPS
1
0.20 ETOPS
2
0.40 ALL
*
0.02
2
0.30 ALL
*
0.02
1
0.20 ALL
*
0.10
1
0.20 ALL
MRB REFERENCE:
26.13.00/01
26.22.00/01
I:
1000 FH
CMP
MRB 9
OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM.
262200-710-801
CMP REFERENCE:
26-2-0000-001
MRB REFERENCE:
26.13.00/01
26.22.00/01
262200-02-1
310 APU FIRE EXTINGUISHING
AV
OPC
I:
48 MO
MRB 8
OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY.
MRB REFERENCE:
26.22.00/09
ACCESS: 313AL
R
262200-03-2
310 APU FIRE EXTINGUISHING
AV
262200-710-802
OPC
I:
48 MO
CMP
MRB 9
OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT.
262200-710-806
CMP REFERENCE:
26-2-0000-002
ACCESS: 313AL
MRB REFERENCE:
26.22.00/07
262200-04-1
310 APU FIRE EXTINGUISHING
AV
DET
I: 14000 FH
MRB 8
DETAILED INSPECTION OF DISTRIBUTION PIPING FOR
CRACKS.
ACCESS: 313AL
262200-05-1
315AL
310 APU FIRE EXTINGUISHING
MRB REFERENCE:
26.22.00/08
316AR
AV
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING
TRIGGER CIRCUIT.
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
262200-200-801
262200-710-804
MRB REFERENCE:
26.22.00/03
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
262200-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 APU FIRE EXTINGUISHING
AV
OPC
I:
48 MO
SOURCE
CMP
MRB 8
OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION.
REFERENCE
262200-710-805
MEN
M/H
APPLICABILITY
2
0.50 ALL
1
1
0.20 NON-ETOPS
0.20
*
0.01
1
1
0.20 ETOPS
0.20
MRB REFERENCE:
26.22.00/02
49.62.00/03-35
*
0.01
262241-280-802
1
0.40 ALL
*
0.02
1
0.30 ETOPS
CMP REFERENCE:
28-2-0000-005
MRB REFERENCE:
26.22.00/10
28.29.00/01
49.62.00/04-35
262200-07-2
210 APU FIRE EXTINGUISHING
AV
OPC
310
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA
MCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF,
6WF).
I:
48 MO
OR
8000 FH
MRB 9
262200-710-803
MRB REFERENCE:
26.22.00/02
49.62.00/03-35
ACCESS: 312AR
R
262200-07-3
210 APU FIRE EXTINGUISHING
AV
OPC
310
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA
MCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF,
6WF).
I:
48 MO
OR
8000 FH
CMP
MRB 9
CMP REFERENCE:
28-2-0000-004
ACCESS: 312AR
262241-01-1
310 APU FIRE EXTINGUISHING
AV
FNC
I:
120 MO
NOTE
262200-710-803
MRB 7,9
REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF
PRESSURE SWITCH SETTING.
MRB REFERENCE:
26.22.00/05
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 313AL
262241-03-1
310 APU FIRE EXTINGUISHING
AV
FNC
I:
6 YE
CMP
FUNCTIONAL TEST OF APU FIRE EXTINGUISHER PRESSURE
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
262241-280-803
CMP REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262241-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
*
0.02
1
0.50 ALL
*
0.02
2
0.50 ALL
*
0.30
1
0.20 ALL
*
0.50
1
0.05 ALL
1
1.50 PRE
PRE
APPLICABILITY
26-2-0000-003
ACCESS: 313AL
310 APU FIRE EXTINGUISHING
AV
DIS
I:
120 MO
MRB 8
DISCARD CARTRIDGE.
262242-920-801
MRB REFERENCE:
26.22.00/11
ACCESS: 313AL
262300-01-1
M/H
* * * * *
SWITCH SETTING
262242-01-1
MEN
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
OPC
I: 12000 FH
MRB 8
262300-710-801
MRB REFERENCE:
26.23.00/04
OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY.
NOTE:
ETOPS RELEVANT
ACCESS: 132SW
262300-02-1
821
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AF
DIS
I:
15 MO
MRB 8
262300-920-802
MRB REFERENCE:
26.23.00/02
DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT.
NOTE:
ETOPS RELEVANT
ACCESS: 132SW
262300-03-1
132WW
821
210 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
OPC
I:
24 MO
MRB 9
MRB REFERENCE:
26.23.00/01
OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW
PRESSURE INDICATION CIRCUIT BY PTT.
262300-04-1
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
AV
262300-710-802
DET
I: 14000 FH
MRB 8
262300-200-803
49144
58269
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-26
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262300-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
MRB REFERENCE:
26.23.00/12
DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND
CHECK VALVE.
PRE 200103
(00-3068)
NOTE:
ETOPS RELEVANT
ACCESS: 132SW
262300-04-2
821
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
DET
DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND
CHECK VALVE.
T: 14000 FH
OR
NOTE
CMR**
MRB 8
I: 14000 FH
262300-05-1
FNC
I: 14000 FH
CMR**
MRB 8
262300-720-803
FUNCTIONAL CHECK OF PRESSURE REDUCER.
CMR REFERENCE:
262300-00001-1-C
NOTE:
ETOPS RELEVANT
MRB REFERENCE:
26.23.00/06
ACCESS: 132SW
262300-06-1
AV
821
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
FNC
I: 14000 FH
1
1.50 POST 49144
OR
POST 58269
OR
POST 200103
(00-3068)
*
0.30
1
0.10 ALL
*
0.30
2
1.93 ALL
CMR REFERENCE:
262300-00002-1-C
821
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
0.30
MRB REFERENCE:
26.23.00/12
NOTE:
- FOR AIRCRAFT ON WHICH MOD 58269 OR MOD 200103 IS
EMBODIED, FIRST ACCOMPLISHMENT MUST BE CARRIED OUT
NO LATER THAN THE AIRCRAFT ACCUMULATING 60000 FH.
- ETOPS RELEVANT
ACCESS: 132SW
262300-200-803
*
MRB 8
262300-200-804
MRB REFERENCE:
26.23.00/09
CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND
OBSTRUCTION.
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262300-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.32
1
1.00 ALL
*
0.30
2
1.50 ALL
*
0.30
1
0.50 ALL
*
0.30
1
1
0.25 IF FIRE
0.25 EXTINGUISHER
* * * * *
ETOPS RELEVANT
ACCESS: 132SW
262341-01-1
821
831
132 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
FNC
I: 10000 FH
MRB 8
262341-280-801
MRB REFERENCE:
26.23.00/03
REMOVE BOTTLE FOR WEIGHT CHECK.
NOTE:
ETOPS RELEVANT
ACCESS: 132SW
262341-02-1
821
132 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
FNC
I:
120 MO
NOTE
MRB 6,9
262341-280-802
MRB REFERENCE:
26.23.00/05
REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF THE
PRESSURE SWITCH SETTING.
NOTE:
- ETOPS RELEVANT
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 132SW
262343-01-1
821
130 LOWER DECK CARGO COMPARTMENT FIRE
EXTINGUISHING (FWD, AFT AND BULK)
AV
DIS
I:
120 MO
MRB 8
262342-920-801
MRB REFERENCE:
26.23.00/11
DISCARD CARTRIDGE UNIT.
NOTE:
ETOPS RELEVANT
ACCESS: 132SW
262400-01-1
821
120 PORTABLE FIRE EXTINGUISHER
200
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
AF
FNC
I:
24 MO
NOTE
MRB 9
262400-280-801
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-26
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262400-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
MEN
M/H
APPLICABILITY
* * * * *
REMOVE BOTTLES FOR WEIGHT CHECK.
MRB REFERENCE:
26.24.00/01
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262400-02-1
REFERENCE
120 PORTABLE FIRE EXTINGUISHER
200
REMOVE BOTTLES FOR HYDROSTATIC TEST.
AF
FNC
I:
CE
NOTE
MRB 9
1000 FH
NOTE
MRB 9
262400-280-802
MRB REFERENCE:
26.24.00/02
WITHOUT PRESSURE
GAUGE IS INSTALLED
1
1
0.25 ALL
0.25 FIRE EXTINGUISHING
SUPPLIERS EXCEPT
"U3061" AND "CE579"
1
0.10 IF LDMCR INSTALLED
1
1
0.20 ALL
0.20
1
0.25 IF LDMCR INSTALLED
IF FIRE
EXTINGUISHER
WITHOUT PRESSURE
GAUGE IS INSTALLED
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262400-03-1
150 PORTABLE FIRE EXTINGUISHER
AF
OPC
I:
OPERATIONAL CHECK AND VISUAL CHECK OF PORTABLE FIRE
EXTINGUISHER ATTACHMENT.
262400-210-804
MRB REFERENCE:
26.24.00/04
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
262400-04-1
262400-05-1
120 PORTABLE FIRE EXTINGUISHER
AF
OPC
200
OPERATIONAL CHECK AND VISUAL CHECK OF PORTABLE FIRE
EXTINGUISHER ATTACHMENT.
I:
150 PORTABLE FIRE EXTINGUISHER
I:
AF
FNC
1000 FH
MRB 9
MRB REFERENCE:
26.24.00/04
24 MO
NOTE
MRB 9
REMOVE BOTTLES FOR WEIGHT CHECK.
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
262400-280-805
MRB REFERENCE:
26.24.00/01
NOTE:
PLANNING:
* * * * *
262400-210-801
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-26
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262400-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262400-06-1
150 PORTABLE FIRE EXTINGUISHER
AF
FNC
I:
CE
NOTE
MRB 9
REMOVE BOTTLES FOR HYDROSTATIC TEST.
262400-10-1
120 PORTABLE FIRE EXTINGUISHER
AV
200
VISUAL CHECK OF THE PORTABLE FIRE EXTINGUISHER
PRESSURE GAUGE READING.
VCK
150 PORTABLE FIRE EXTINGUISHER
VCK
AV
1
0.25 IF LDMCR INSTALLED
ALL FIRE
EXTINGUISHING
SUPPLIERS EXCEPT
"U3061" AND "CE579"
1
1
0.10 IF FIRE
0.10 EXTINGUISHER WITH
PRESSURE GAUGE IS
INSTALLED
1
0.05 IF LDMCR INSTALLED
IF FIRE
EXTINGUISHER WITH
PRESSURE GAUGE IS
INSTALLED
1
1
0.20 IF FIRE
0.20 EXTINGUISHER P/N
892480 INSTALLED
MRB REFERENCE:
26.24.00/02
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262400-09-1
262400-280-806
I:
1000 FH
MRB 9
262400-220-802
MRB REFERENCE:
26.24.00/05
I:
1000 FH
NOTE
MRB 9
VISUAL CHECK OF THE PORTABLE FIRE EXTINGUISHER
PRESSURE GAUGE READING.
262400-220-804
MRB REFERENCE:
26.24.00/05
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED.
262400-11-1
120 PORTABLE FIRE EXTINGUISHER
200
WEIGHT CHECK OF PROPELLANT GAS CARTRIDGE.
AV
FNC
I:
12 MO
NOTE
MRB 9
262400-220-803
MRB REFERENCE:
26.24.00/06
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262400-11-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262400-12-1
150 PORTABLE FIRE EXTINGUISHER
AV
FNC
I:
12 MO
NOTE
MRB 9
WEIGHT CHECK OF PROPELLANT GAS CARTRIDGE.
262400-220-805
1
0.10 IF LDMCR INSTALLED
IF FIRE
EXTINGUISHER P/N
892480 INSTALLED
1
1
0.20 IF FIRE
0.20 EXTINGUISHER FROM
SUPPLIER "U3061"
INSTALLED
OR
IF FIRE
EXTINGUISHER FROM
SUPPLIER "CE579"
INSTALLED
1
0.10 IF LDMCR WITH FIRE
EXTINGUISHER FROM
SUPPLIER "U3061"
INSTALLED
OR
IF LDMCR WITH FIRE
EXTINGUISHER FROM
SUPPLIER "CE579"
INSTALLED
1
0.20 ALL
1
1
0.20 ALL
0.20
MRB REFERENCE:
26.24.00/06
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
R
262400-13-1
120 PORTABLE FIRE EXTINGUISHER
200
DISCARD PORTABLE FIRE EXTINGUISHER.
AV
DIS
I:
CE
NOTE
MRB 9
CE
NOTE
MRB 9
262400-920-801
MRB REFERENCE:
26.24.00/07
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
R
262400-14-1
150 PORTABLE FIRE EXTINGUISHER
AV
DIS
I:
DISCARD PORTABLE FIRE EXTINGUISHER.
MRB REFERENCE:
26.24.00/07
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262500-01-1
200 LAVATORY FIRE EXTINGUISHING
AV
OPC
I:
24 MO
MRB 9
CHECK PRESSURE OF EXTINGUISHING AGENT.
262500-03-1
100 LAVATORY FIRE EXTINGUISHING
200
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
262400-920-802
262500-280-803
MRB REFERENCE:
26.25.00/01
AV
DET
I:
48 MO
MRB 9
262500-220-802
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262500-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
200 LAVATORY FIRE EXTINGUISHING
AF
FNC
I:
72 MO
MRB 9
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
250 INSTALLED) (CREW REST ROOM - UNDERFLOOR)
AV
OPC
I: 12000
CRR FH
MRB 8
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
262500-280-804
AV
DIS
I:
MRB 8
120 MO
AV
FNC
262800-750-801
MRB REFERENCE:
26.28.00/02
1
2.00 ALL
1
1
0.40 IF AUTOMATIC
0.40 ACTUATION OF LDMCR
FIRE EXTINGUISHING
SYSTEM INSTALLED
262842-920-801
1
0.25 IF LDMCR INSTALLED
1
1.00 IF LDMCR INSTALLED
1
0.50 IF LDMCR INSTALLED
MRB REFERENCE:
26.28.00/03
DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE IN THE
LDMCR.
262800-04-1
APPLICABILITY
MRB REFERENCE:
26.25.00/02
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING
CIRCUIT IN THE LDMCR.
262800-03-1
M/H
MRB REFERENCE:
26.25.00/03
REMOVE BOTTLE FOR WEIGHT CHECK.
262800-02-1
MEN
* * * * *
DETAILED INSPECTION OF LAVATORY FIRE EXTINGUISHER FOR
SIGNS OF LEAKAGE/DISCHARGE.
262541-01-1
REFERENCE
I:
120 MO
NOTE
MRB 8
262841-280-802
MRB REFERENCE:
26.28.00/04
REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF THE
PRESSURE SWITCH SETTING IN THE LDMCR.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
262800-05-1
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
AF
OPC
I:72CRR MO
MRB 8
MRB REFERENCE:
26.28.00/05
OPERATIONAL CHECK OF THE FIRE EXTINGUISHING LINES FOR
OBSTRUCTION IN THE LDMCR.
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
262800-210-801
REV. DATE: JUL 01/21
SECTION:
2 -26
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
262800-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
AF
OPC
I:2000 CRR
FH
SOURCE
MRB 8
REFERENCE
262800-710-802
ACCESS: 251EH
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
AF
OPC
I: 38000 FH
OR
48 CRR MO
CMR*
MRB 9
OPERATIONAL CHECK OF MANUAL FIRE EXTINGUISHING
CIRCUIT IN THE LDMCR.
262800-08-1
150 AUXILIARY AREAS FIRE EXTINGUISHING (IF
INSTALLED) (CREW REST ROOM - UNDERFLOOR)
AV
E N D
SYSTEMS, APU AND POWER PLANT : FIRE PROTECTION
APPLICABILITY
1
0.05 IF LDMCR INSTALLED
*
0.01
262800-710-804
1
0.20 IF MANUAL ACTUATION
OF LDMCR FIRE
EXTINGUISHING
SYSTEM INSTALLED
1
0.10 IF LDMCR INSTALLED
CMR REFERENCE:
262800-00001-1-C
MRB REFERENCE:
26.28.00/07
OPC
I:24CRR MO
MRB 8
262800-710-806
MRB REFERENCE:
26.28.00/08
OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT
IN THE LDMCR.
* * * * *
M/H
MRB REFERENCE:
26.28.00/06
OPERATIONAL CHECK OF SQUIB FUNCTIONALITY IN THE
LDMCR.
262800-07-1
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-26
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
271400-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AILERON AND HYDRAULIC ACTUATION
AF
OPC
I: 12000 FH
SOURCE
MRB 8
OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY
BITE.
REFERENCE
271400-740-802
MEN
M/H
APPLICABILITY
1
0.20 PRE 49144
PRE 200103
(00-3068)
1
0.20 POST 49144
OR
POST 200103
(00-3068)
1
1
0.30 ALL
0.30
*
*
0.40
0.40
1
1
1
0.60 ALL
0.60
0.60
*
2.70
*
2.70
1
1
0.20 ALL
0.20
MRB REFERENCE:
27.14.00/01
29.10.00/12
NOTE:
ETOPS RELEVANT
271400-01-2
210 AILERON AND HYDRAULIC ACTUATION
AF
OPC
OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY
BITE.
NOTE:
- FOR AIRCRAFT ON WHICH MOD 200103 IS EMBODIED, FIRST
ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN
THE AIRCRAFT ACCUMULATING 60000 FH.
- ETOPS RELEVANT
271400-02-1
575 AILERON AND HYDRAULIC ACTUATION
675
OPERATIONAL CHECK OF AILERON SERVO CONTROL
ACCUMULATOR PISTON POSITION.
ACCESS: 575AB
675AB
271400-03-1
OPC
I: 12000 FH
I: 34000 FH
271400-740-802
CMR REFERENCE:
271400-00001-1-C
MRB REFERENCE:
27.14.00/01
29.10.00/12
MRB 8
271400-210-801
575CB
675CB
575BB
591DB
675BB
691DB
575CB
592AB
675CB
692AB
575DB
592BB
675DB
692BB
591AB
592CB
691AB
692CB
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
I: 30000 FH
MRB 8
271400-200-801
MRB REFERENCE:
27.14.00/03
591BB
592DB
691BB
692DB
575 AILERON AND HYDRAULIC ACTUATION
675
LUBRICATION OF AILERON HINGE BEARINGS.
* * * * *
CMR**
MRB 8
MRB REFERENCE:
27.14.00/02
210 AILERON AND HYDRAULIC ACTUATION
AF
FNC
575
675 CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR
EXCESSIVE PLAY AND GENERAL CONDITION.
ACCESS: 575AB
591CB
675AB
691CB
271400-04-1
AF
T: 12000 FH
OR
NOTE
AF
LUB
I:
7500 FH
OR
18 MO
MRB 9
122227-640-807
MRB REFERENCE:
27.14.00/04
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
271400-04-1
ZONE
* * * * *
ACCESS: 575AB
591AB
592CB
675AB
691AB
692CB
271400-05-1
C O N T I N U E
575AT
591BB
592DB
675AT
691BB
692DB
SOURCE
575DB
592BB
*
3.60
675BB
691CB
675BT
691DB
675CB
692AB
675DB
692BB
*
3.60
1
1
0.10 POST 45512
0.10 (27-3054)
OR
POST 47433
0.40 (27-3075)
0.40 OR
POST 48221
(00-3033)
I:
7500 FH
OR
18 MO
MRB 8
I:
72 MO
MRB 5,9
272100-210-801
MRB REFERENCE:
27.21.00/08
162ZW
312AR
AF
DET
I:
72 MO
OR
24000 FH
MRB 8
272100-210-802
AF
DETAILED INSPECTION OF DUPLICATED CONTROL RODS OF
RUDDER MECHANICAL CONTROL.
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
DET
I:
72 MO
OR
20000 FH
*
*
1
1
*
1.00 A330-200
1.00 PRE 49144
OR
A330-300
>99.9 PRE 49144
*
*
0.03
0.04
1
0.20 A330-300
PRE 49144
*
2.30
1
0.20 A330-200
PRE 49144
MRB REFERENCE:
27.21.00/07
325ER
325 RUDDER MECHANICAL CONTROL
* * * * *
122227-640-811
MRB REFERENCE:
27.14.00/05
575CB
675CB
DETAILED INSPECTION OF DUPLICATED CONTROL RODS OF
RUDDER MECHANICAL CONTROL.
272100-02-2
APPLICABILITY
575CB
592AB
325 RUDDER MECHANICAL CONTROL
ACCESS: 325DL
M/H
575BT
591DB
PREP.: CEILING PANELS Z130;
CEILING PANELS Z150;
CEILING PANELS Z160;
FLOOR PANELS Z250;
272100-02-1
MEN
575BB
591CB
100 RUDDER MECHANICAL CONTROL
AF
DET
310
DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL.
ACCESS: 132AZ
311AZ
REFERENCE
* * * * *
575 AILERON AND HYDRAULIC ACTUATION
AF
LUB
675
LUBRICATION OF AILERON SERVO CONTROL ROLLER BEARINGS.
ACCESS: 575AB
675AB
272100-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MRB 8
272100-210-802
MRB REFERENCE:
27.21.00/07
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272100-02-2
ZONE
* * * * *
ACCESS: 325NL
272100-03-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
325NR
AF
FNC
I:
48 MO
MRB 9
FUNCTIONAL CHECK OF CABLE TENSION REGULATOR POINTER
WITHIN LIMITS.
272100-04-1
272100-200-801
811
325 RUDDER MECHANICAL CONTROL
AF
OPC
I: 34000 FH
MRB 8
272100-19-1
210 RUDDER MECHANICAL CONTROL
AF
LUB
I:
24 MO
I:
210 RUDDER MECHANICAL CONTROL
I: 24000 FH
MRB 6
EL
OPC
72 MO
MRB 6
1
0.30 A330-200
PRE 49144
OR
A330-300
PRE 49144
0.06
272100-710-801
C O N T I N U E D
1
*
0.30 A330-200
PRE 49144
OR
A330-300
0.50 PRE 49144
272143-600-801
1
0.20 ALL
272100-210-805
1
1
1.00 A330-200
1.00 POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
1
0.20 A330-200
POST 49144
OR
A330-300
POST 49144
MRB REFERENCE:
27.21.00/18
MRB 9
OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY
CHANNEL.
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
APPLICABILITY
MRB REFERENCE:
27.21.00/16
120 RUDDER MECHANICAL CONTROL
AF
DET
210
DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT.
* * * * *
3.60
MRB REFERENCE:
27.21.00/12
LUBRICATION OF THE RUDDER PEDALS ADJUSTMENT
MECHANISM.
272100-18-1
*
*
ACCESS: 325BL
272100-05-1
M/H
MRB REFERENCE:
27.21.00/04
OPERATIONAL CHECK OF CENTERING MECHANISM.
R
MEN
* * * * *
121 RUDDER MECHANICAL CONTROL
ACCESS: 312AR
REFERENCE
272200-710-806
MRB REFERENCE:
27.21.00/19
27.90.00/18
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272100-19-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-200F
OR
A330-800
OR
A330-900
272100-20-1
122 RUDDER MECHANICAL CONTROL
AF
OPC
I:
4 C
MRB 9
OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL.
MRB REFERENCE:
27.21.00/20
ACCESS: 811
N
272100-21-1
310 RUDDER MECHANICAL CONTROL
AF
LUB
I:
36 MO
MRB 5
LUBRICATION OF RUDDER CONTROL CABLES (AFT SECTION).
325 RUDDER MECHANICAL CONTROL
AF
FNC
I:
FUNCTIONAL CHECK OF RUDDER SERVO-CONTROLS FOR FREE
PLAY AND SYNCHRONIZATION FOLLOWED BY SPRING-ROD
REMOVAL FOR WORKSHOP CHECK.
ACCESS: 311AZ
272200-01-1
312AR
325BL
210 RUDDER MECHANICAL CONTROL
48 MO
OR
24000 FH
MRB 8
272149-200-801
325DL
AF
OPC
I:
4 C
1
*
1
*
MRB 9
272200-710-801
MRB REFERENCE:
27.21.00/09
REV. DATE: JUL 01/21
SECTION:
2-27
0.20 A330-200
POST 49144
OR
A330-300
0.05 POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
TBD A330-200
PRE 49144
OR
A330-300
0.01 PRE 49144
1
1.50 A330-200
PRE 49144
OR
A330-300
PRE 49144
*
1.24
2
0.20 A330-200
PRE 49144
OR
A330-300
PRE 49144
MRB REFERENCE:
27.21.00/11
27.24.00/04
OPERATIONAL CHECK OF AP ARTIFICIAL FEEL SPRING ROD.
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
122227-640-818
MRB REFERENCE:
27.21.00/21
ACCESS: 312AR
272149-01-1
272200-710-808
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272200-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 RUDDER MECHANICAL CONTROL
AF
OPC
I: 24000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL.
272300-01-1
210 RUDDER MECHANICAL CONTROL
AF
OPC
311 RUDDER MECHANICAL CONTROL
I: 24000 FH
MRB 9
AF
DET
I:
72 MO
OR
2000 FH
CMR**
MRB 8
AF
DET
I:
DETAILED INSPECTION OF CONTROL ROD (ITEM 220 IN IPC
272147-1A) IN PTLU LINKAGE.
72 MO
OR
20000 FH
CMR**
MRB 8
210 RUDDER HYDRAULIC ACTUATION
AF
OPC
I:
800 FH
MRB 8
OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH
INDIVIDUAL HYDRAULIC SYSTEMS.
0.15 A330-200
PRE 49144
OR
A330-300
PRE 49144
1
0.20 A330-300
PRE 41800
POST 44442
(27-3069)
PRE 49144
0.01
MRB REFERENCE:
27.21.00/15
*
272300-210-803
1
MRB REFERENCE:
27.21.00/15
*
272400-710-801
1
MRB REFERENCE:
27.24.00/02
29.10.00/08
NOTE:
ETOPS RELEVANT
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
1
CMR REFERENCE:
272100-00002-2-C
ACCESS: 312AR
272400-01-1
272300-210-803
REV. DATE: JUL 01/21
SECTION:
2 -27
APPLICABILITY
0.10 A330-200
PRE 49144
OR
A330-300
PRE 49144
CMR REFERENCE:
272100-00002-1-C
ACCESS: 312AR
311 RUDDER MECHANICAL CONTROL
272300-710-801
M/H
1
MRB REFERENCE:
27.21.00/06
DETAILED INSPECTION OF CONTROL ROD (ITEM 220 IN IPC
272147-1A) IN PTLU LINKAGE.
272300-04-3
272200-710-803
MEN
MRB REFERENCE:
27.21.00/05
OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL
LIMITATION UNITS STANDBY CHANNEL.
272300-04-2
REFERENCE
0.20 A330-200
POST 44442
(27-3069)
PRE 49144
OR
0.01 A330-300
POST 41800
POST 44442
(27-3069)
PRE 49144
0.25 A330-200
PRE 49144
OR
A330-300
PRE 49144
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272400-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
325 RUDDER HYDRAULIC ACTUATION
AF
LUB
I:
LUBRICATION OF RUDDER HINGE BEARING NO4.
7500 FH
OR
18 MO
SOURCE
MRB 9
210 RUDDER HYDRAULIC ACTUATION
AF
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF RUDDER SERVO CONTROL JAMMING
DEVICE.
272400-05-2
325 RUDDER HYDRAULIC ACTUATION
AF
272400-06-1
312AR
325NL
326LL
326ML
CHK
I: 33000 FH
CMR**
AF
LUB
I:
18 MO
OR
7500 FH
MRB 8
122227-640-810
LUB
I:
LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER
BEARING (RUDDER SIDE).
18 MO
OR
7500 FH
MRB 8
122227-640-810
325 RUDDER HYDRAULIC ACTUATION
AF
LUB
LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER
BEARING (RUDDER SIDE).
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
*
0.70
1
0.10 A330-200
PRE 49144
OR
A330-300
PRE 49144
1
3.00 A330-200
PRE 49144
*
3.14
1
0.20 A330-200
POST 44647
PRE 49144
OR
A330-200
2.50 POST 49144
OR
A330-200F
I:
18 MO
OR
7500 FH
1
0.30 A330-300
POST 49144
*
0.70
1
0.30 A330-800
OR
A330-900
MRB REFERENCE:
27.24.00/06
ACCESS: 325DL
272400-06-3
0.10 A330-300
OR
A330-900
*
AF
APPLICABILITY
1
MRB REFERENCE:
27.24.00/06
325NL
325 RUDDER HYDRAULIC ACTUATION
M/H
CMR REFERENCE:
272400-00001-2-C
LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER
BEARING (RUDDER SIDE).
272400-06-2
272451-200-801
326NL
325 RUDDER HYDRAULIC ACTUATION
ACCESS: 325DL
272400-710-803
MEN
MRB REFERENCE:
27.24.00/03
REMOVE RUDDER SERVO CONTROL FOR WORKSHOP CHECK OF
INTERNAL SEALS
ACCESS: 311AZ
122255-600-801
MRB REFERENCE:
27.24.00/01
ACCESS: 325DL
272400-04-1
REFERENCE
MRB 8
122227-640-810
MRB REFERENCE:
27.24.00/06
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272400-06-3
ZONE
* * * * *
ACCESS: 325DL
272400-07-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
REFERENCE
325NL
325 RUDDER HYDRAULIC ACTUATION
AF
LUB
I:
18 MO
OR
7500 FH
MRB 9
122255-600-802
*
2.50
1
0.10 A330-200
OR
A330-200F
OR
1.60 A330-800
MRB REFERENCE:
27.24.00/07
ACCESS: 325PL
210 RUDDER HYDRAULIC ACTUATION
M/H
*
AF
OPC
I: 12000 FH
OPERATIONAL CHECK OF RUDDER DAMPING MEASUREMENT BY
BITE.
CMR**
MRB 9
272400-740-802
1
0.20 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
1
0.30 A330-300
PRE 49144
1
2.00 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
CMR REFERENCE:
272400-00002-1-C
MRB REFERENCE:
27.24.00/08
272400-10-1
210 RUDDER HYDRAULIC ACTUATION
APPLICABILITY
* * * * *
LUBRICATION OF RUDDER HINGE BEARING NO 6.
272400-08-1
MEN
AF
FNC
I: 12000 FH
FUNCTIONAL CHECK OF INDIVIDUAL RUDDER SERVOCONTROLS.
CMR**
MRB 9
272400-720-801
CMR REFERENCE:
272400-00003-1-C
MRB REFERENCE:
27.24.00/10
272400-11-1
325 RUDDER HYDRAULIC ACTUATION
AF
FNC
I: 34000 FH
MRB 8
FUNCTIONAL CHECK OF RUDDER SERVO CONTROL AND HINGE
BEARINGS FOR EXCESSIVE PLAY AND GENERAL CONDITION.
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
272400-200-801
MRB REFERENCE:
27.24.00/11
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
272600-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 RUDDER MECHANICAL CONTROL
AF
OPC
I:
2400 FH
SOURCE
CMR**
MRB 8
OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE.
REFERENCE
272600-740-802
MEN
272600-05-4
210 RUDDER MECHANICAL CONTROL
AF
0.20 A330-200
PRE 49144
PRE 200630
OR
A330-300
PRE 49144
PRE 200630
1
0.20 A330-200
PRE 49144
POST 200630
OR
A330-300
PRE 49144
POST 200630
1
0.10 POST 49144
OR
POST 200103
(00-3068)
1
0.10 PRE 49144
PRE 200103
(00-3068)
1
1
1
0.40 ALL
0.40
0.40
CMR REFERENCE:
272100-00001-1-C
OPC
I:
3200 FH
MRB 8
OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE.
273400-01-1
210 ELEVATOR AND HYDRAULIC ACTUATION
AF
272600-740-802
MRB REFERENCE:
27.21.00/13
OPC
OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY
BITE.
T: 12000 FH
OR
NOTE
CMR**
MRB 8
273400-740-802
APPLICABILITY
1
MRB REFERENCE:
27.21.00/13
N
M/H
CMR REFERENCE:
273400-00001-1-C
I: 12000 FH
NOTE:
- FOR AIRCRAFT ON WHICH MOD 200103 IS EMBODIED, FIRST
ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE
AIRCRAFT ACCUMULATING 60000 FH.
273400-01-2
210 ELEVATOR AND HYDRAULIC ACTUATION
AF
OPC
MRB REFERENCE:
27.34.00/01
I: 12000 FH
MRB 8
OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY
BITE.
273400-02-1
210 ELEVATOR AND HYDRAULIC ACTUATION
AF
FNC
330
340 CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR
EXCESSIVE PLAY AND GENERAL CONDITION.
ACCESS: 334AB
334GB
335FB
344AB
345AB
273400-740-802
MRB REFERENCE:
27.34.00/01
I: 30000 FH
MRB 8
273400-200-801
MRB REFERENCE:
27.34.00/02
334BB
335AB
334CB
335BB
334DB
335CB
334EB
335DB
334FB
335EB
*
6.25
344BB
345BB
344CB
345CB
344DB
345DB
344FB
345EB
344GB
345FB
*
5.75
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
273400-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
330 ELEVATOR AND HYDRAULIC ACTUATION
340
OPERATIONAL CHECK OF ELEVATOR SERVO CONTROL
ACCUMULATOR PISTON POSITION.
AF
OPC
I: 34000 FH
SOURCE
MRB 8
REFERENCE
273400-210-801
330 ELEVATOR AND HYDRAULIC ACTUATION
AF
LUB
340
LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING.
I:
7500 FH
OR
18 MO
MRB 8
122227-640-814
MRB REFERENCE:
27.34.00/04
ACCESS: 334CB
344CB
274000-01-1
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
M/H
APPLICABILITY
1
1
0.20 ALL
0.20
*
*
0.50
0.50
1
1
*
*
0.10 POST 47674
0.10 (27-3076)
OR
POST 49586
0.50 (27-3076)
0.50
1
0.30 ALL
*
0.01
1
1
0.25 ALL
0.25
*
0.01
MRB REFERENCE:
27.34.00/03
ACCESS: 334CB
344CB
273400-06-1
MEN
AF
DET
I: 12000 FH
MRB 8
DETAILED INSPECTION OF FOLLOWING ITEMS OF TRIMMABLE
HORIZONTAL STABILIZER ACTUATOR:
- FAIL SAFE NUT
- UPPER AND LOWER ATTACHMENTS (PRIMARY AND SECONDARY)
- NO-BACK HOUSING
274400-210-801
MRB REFERENCE:
27.40.00/06
27.40.00/07
27.40.00/08
NOTE:
PARTIAL CREDIT CAN BE TAKEN FROM LAST ACCOMPLISHMENT
OF MPD TASK 274000-04-1 WHEN PERFORMED AT THE SAME
TIME (ONLY LOWER ATTACHMENTS AND FAIL SAFE NUT
INSPECTION IS REQUIRED)
ACCESS: 312AR
274000-04-1
311 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
312
DETAILED INSPECTION OF UPPER THS ACTUATOR ATTACHMENT
(PRIMARY AND SECONDARY) AND NO-BACK HOUSING.
T:
I:
NOTE:
NO SHORT-TERM EXTENSION IS ALLOWED.
1000 FC
OR
4000 FH
SEMR
274400-210-805
SEMR REFERENCE:
274400-00004-1-E
1000 FC
OR
4000 FH
ACCESS: 312AR
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
274000-18-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
310
OPERATIONAL CHECK OF THSA CHECKABLE SHEAR PIN.
OPC
I: 12000 FH
SOURCE
CMR*
MRB 9
REFERENCE
274451-710-801
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
310
OPERATIONAL CHECK OF THSA LOAD SENSING DEVICE.
OPC
I: 12000 FH
MRB 8
274451-710-802
274000-20-1
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
I: 24000 FH
MRB 9
OPERATIONAL CHECK OF THS ACTUATOR OVERRIDE MECHANISM.
R
274100-01-1
120 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
LUB
310
LUBRICATION OF THS MECHANICAL CONTROL CHAINS (FWD AND
AFT SECTIONS) AND CABLES (AFT SECTION).
ACCESS: 312AR
274100-02-1
274400-710-806
I:
36 MO
MRB 6
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
0.01
2
2
0.15 POST 206264
0.15 (27-3234)
*
0.01
1
TBD ALL
122227-640-802
1
1
0.20 ALL
0.20
*
0.06
1
1
1
0.40 ALL
0.40
0.40
MRB REFERENCE:
27.40.00/09
I:
4 C
MRB 6
274100-210-801
MRB REFERENCE:
27.40.00/14
PREP.: FLOOR PANELS Z250;
SEATS AND FURNISHINGS Z250;
C O N T I N U E D
*
MRB REFERENCE:
27.40.00/20
811
100 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
210
310 DETAILED INSPECTION OF THS MECHANICAL CONTROL LOOP.
* * * * *
0.15 IF BOTH MODIFIED
0.15 THSA AND ELECTRICAL
HARNESSES ARE
INSTALLED, SEE NOTE
MRB REFERENCE:
27.40.00/19
ACCESS: 312AR
N
APPLICABILITY
MRB REFERENCE:
27.40.00/18
ACCESS: 312AR
274000-19-1
M/H
1
1
CMR REFERENCE:
274000-00003-1-C
NOTE:
THSA MODIFICATIONS AND ASSOCIATED SERVICE BULLETINS:
- PRODUCTION SOLUTION: 55780
- RETROFIT SOLUTION: 54880 (27-3137) OR 54881
(27-3143) OR (27-3181)
ELECTRICAL HARNESSES MODIFICATIONS AND ASSOCIATED
SERVICE BULLETINS:
- PRODUCTION SOLUTION: (52269 AND 56056)
- RETROFIT SOLUTION: (52270 AND 56057 AND 58493
(92-3046)) OR (52359 AND 56057 AND 58493 (92-3046)).
R
MEN
*
>99.9
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
274100-02-1
ZONE
* * * * *
ACCESS: 131BC
131TC
151HC
312AR
274100-04-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
131FC
131VC
151KC
131KC
132AZ
151PC
SOURCE
REFERENCE
MEN
M/H
*
3.28
*
0.01
1
0.10 ALL
*
0.01
1
1
0.80 ALL
0.80
MRB REFERENCE:
27.40.00/04
*
0.01
274400-710-802
1
0.20 ALL
1
0.10 ALL
*
0.01
1
0.30 ALL
* * * * *
131MC
151BC
161BC
131PC
151DC
161EC
131RC
151FC
162ZW
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
FNC
I:
48 MO
MRB 6
FUNCTIONAL CHECK OF MOVABLE INDEX ON THS CABLE
TENSION COMPENSATOR SCALE WITHIN LIMITS.
274100-220-802
MRB REFERENCE:
27.40.00/10
ACCESS: 312AR
274400-01-1
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
310
OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION
DEVICE.
I:
6900 FH
CMR*
MRB 8
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
274400-710-801
CMR REFERENCE:
274000-00001-1-C
ACCESS: 312AR
274400-02-1
APPLICABILITY
I:
800 FH
CMR**
MRB 8
OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL
HYDRAULIC SYSTEMS.
CMR REFERENCE:
274000-00002-1-C
MRB REFERENCE:
27.40.00/01
274400-03-1
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
SVC
I:
6400 FH
MRB 6,9
CHECK OIL LEVEL OF THS ACTUATOR GEARBOX.
274451-210-801
MRB REFERENCE:
27.40.00/03
ACCESS: 312AR
274400-04-1
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
FNC
I:
4 C
MRB 9
FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE-OFF BRAKE
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
274454-720-801
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
274400-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
I: 12000 FH
MRB 9
CHECK MAGNETIC CHIP DETECTOR OF THS ACTUATOR GEARBOX.
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
274451-210-802
MRB REFERENCE:
27.40.00/05
ACCESS: 312AR
I: 15000 FH
MRB 8
DETAILED INSPECTION OF WEAR INDICATOR OF THS ACTUATOR
NO-BACK SYSTEM.
274451-220-802
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
I: 34000 FH
MRB 8
OPERATIONAL CHECK OF THS ACTUATOR NO-BACK SYSTEM.
274400-710-803
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
FNC
I: 16000 FH
MRB 8
CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT
(PRIMARY AND SECONDARY LOAD PATH).
274451-220-801
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
LUB
LUBRICATION OF THS ACTUATOR BALL SCREW NUT.
NOTE:
- NO SHORT-TERM EXTENSION IS ALLOWED.
- PRIOR TO THIS TASK PERFORM EITHER TASK 274400-13-1
OR 274400-14-1 (IF APPLICABLE).
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
0.20 ALL
*
0.01
1
0.10 ALL
*
0.01
1
0.30 ALL
*
0.01
1
0.40 ALL
*
0.01
1
0.50 ALL
MRB REFERENCE:
27.40.00/12
ACCESS: 312AR
274400-09-1
1
MRB REFERENCE:
27.40.00/13
ACCESS: 312AR
274400-08-1
0.01
MRB REFERENCE:
27.40.00/11
ACCESS: 312AR
274400-07-1
*
APPLICABILITY
27.40.00/15
ACCESS: 312AR
274400-06-1
M/H
* * * * *
(CHECK OF STATIC TORQUE).
274400-05-1
MEN
T:
1000 FH
NOTE
I:
1000 FH
NOTE
MRB 8
SEMR
122227-640-801
MRB REFERENCE:
27.40.00/02
SEMR REFERENCE:
274400-00002-1-E
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
274400-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
VCK
I:
3000 FH
MRB 9
VISUAL CHECK OF THS ACTUATOR DRAIN COLLECTING
CONTAINER ASSEMBLY INCLUDING HOSES AND HYDRAULIC
FLUID LEVEL.
274400-210-803
*
0.01
1
0.10 POST 43683
OR
POST 45578
*
0.01
1
0.40 IF P/N 47147-500
INSTALLED
OR
IF P/N 47172-300
INSTALLED
*
0.01
1
1
0.20 PRE 56056
0.20 PRE SB 92-3046
P/N 47172-500
INSTALLED
OR
PRE 56056
PRE SB 92-3046
P/N 47172-520
INSTALLED
MRB REFERENCE:
27.40.00/16
ACCESS: 312AR
274400-13-1
M/H
APPLICABILITY
* * * * *
ACCESS: 312AR
274400-10-1
MEN
310 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
DETAILED INSPECTION OF THSA BALLSCREW ASSY FOR
INTEGRITY OF PRIMARY AND SECONDARY LOAD PATH AND
CHECK THE GAP AT SECONDARY NUT TRUNNION.
T:
700 FH
NOTE
I:
700 FH
NOTE
SEMR
274451-210-805
SEMR REFERENCE:
274400-00001-1-E
NOTE:
- THIS TASK MUST BE PERFORMED PRIOR TO TASK
274400-09-1.
- NO SHORT TERM EXTENSION IS ALLOWED.
- FOR 100% THRESHOLD:
IN COMPUTING THE LIFE ACCUMULATED BY THE THSA FOR
COMPLIANCE WITH THE THRESHOLD, CALCULATIONS MUST
INCLUDE FLIGHT HOURS SINCE THE INITIAL ENTRY INTO
SERVICE OR SINCE 17-AUG-2002, WHICHEVER OCCURS LATER.
ACCESS: 312AR
274400-14-1
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
310
DETAILED INSPECTION OF THE BALL SCREW ASSEMBLY FOR
INTEGRITY OF THE PRIMARY AND SECONDARY LOAD PATH AND
CHECK THE CHECKABLE SHEAR PINS (CSP).
T:
700 FH
NOTE
I:
700 FH
NOTE
SEMR
274451-210-810
SEMR REFERENCE:
274400-00001-2-E
NOTE:
- THIS TASK MUST BE PERFORMED PRIOR TO TASK
274400-09-1.
- NO SHORT TERM EXTENSION ALLOWED.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
274400-14-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
M/H
*
0.01
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
310
DETAILED INSPECTION OF THE BALL SCREW ASSEMBLY FOR
INTEGRITY OF THE PRIMARY AND SECONDARY LOAD PATH AND
CHECK THE CHECKABLE SHEAR PINS (CSP).
T:
700 FH
NOTE
I:
700 FH
NOTE
SEMR
274451-210-810
1
1
0.20 PRE 56056
0.20 PRE SB 92-3046
P/N 47172-510
INSTALLED
OR
PRE 56056
PRE SB 92-3046
P/N 47172-530
INSTALLED
OR
PRE 56056
0.01 PRE SB 92-3046
P/N 47172-540
INSTALLED
SEMR REFERENCE:
274400-00001-3-E
NOTE:
- THIS TASK MUST BE PERFORMED PRIOR TO TASK
274400-09-1.
- NO SHORT TERM EXTENSION ALLOWED.
ACCESS: 312AR
274400-14-4
210 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
DET
310
DETAILED INSPECTION OF THE BALL SCREW ASSEMBLY FOR
INTEGRITY OF THE PRIMARY AND SECONDARY LOAD PATH AND
CHECK THE CHECKABLE SHEAR PINS (CSP).
*
T:
700 FH
NOTE
I:
700 FH
NOTE
SEMR
274451-210-810
1
1
0.20 PRE 56056
0.20 PRE SB 92-3046
P/N 47147-700
INSTALLED
OR
PRE 56056
PRE SB 92-3046
P/N 47147-710
INSTALLED
*
0.01
SEMR REFERENCE:
274400-00001-4-E
NOTE:
- THIS TASK MUST BE PERFORMED PRIOR TO TASK
274400-09-1.
- NO SHORT TERM EXTENSION ALLOWED.
ACCESS: 312AR
R
274400-16-1
APPLICABILITY
* * * * *
ACCESS: 312AR
274400-14-3
MEN
311 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
RST
312
REMOVE COMPLETE THSA FOR NO-BACK BRAKE (NBB) CARBON
DISK DISCARD AND REPLACE WITH SERVICEABLE THSA UNIT.
T:
8500 FC
NOTE
SEMR
274451-920-801
I:
8500 FC
SEMR REFERENCE:
274400-00003-1-E
REV. DATE: JUL 01/21
SECTION:
1
1
24.00 IF P/N 47147-710
24.00 INSTALLED
NOTE:
THE THRESHOLD OF 8500 FC IS THE TIME SINCE RETROFIT
IN PNR 47147-710.
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
2 -27
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
274400-16-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
311 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
RST
312
REMOVE COMPLETE THSA FOR NO-BACK BRAKE (NBB) CARBON
DISK DISCARD AND REPLACE WITH SERVICEABLE THSA UNIT.
T:
8500 FC
NOTE
I:
8500 FC
T:
8500 FC
NOTE
I:
8500 FC
T:
24 MO
OR
2300 FC
SOURCE
SEMR
REFERENCE
274451-920-801
MEN
274400-16-3
311 TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
RST
312
REMOVE COMPLETE THSA FOR NO-BACK BRAKE (NBB) CARBON
DISK DISCARD AND REPLACE WITH SERVICEABLE THSA UNIT.
24.00 IF P/N 47172-500
24.00 INSTALLED
OR
IF P/N 47172-510
INSTALLED
OR
IF P/N 47172-520
INSTALLED
OR
IF P/N 47172-530
INSTALLED
1
1
24.00 IF P/N 47147-700
24.00 INSTALLED
SEMR REFERENCE:
274400-00003-2-E
SEMR
274451-920-801
APPLICABILITY
1
1
NOTE:
- FOR THSA PNRS 47172-500, 47172-510 AND 47172-520
THRESHOLD OF 8500 FC IS THE TIME SINCE NEW
- FOR THSA PNR 47172-530 THE THRESHOLD OF 8500 FC IS
THE TIME SINCE NEW FOR THSA ORIGINALLY MANUFACTURED
AS PNR 47172-530 OR THE TIME SINCE RETROFIT INTO
PNR 47172-530 OR THE TIME SINCE NEW FOR SPECIFIC
THSA PNR 47172-530 SNR 503, WHICH WAS RETROFITTED
INTO PNR 47172-530 WITHOUT NBB DISKS REPLACEMENT
N
M/H
SEMR REFERENCE:
274400-00003-3-E
NOTE:
THE THRESHOLD OF 8500 FC IS THE TIME SINCE NEW
R
275000-02-1
574 FLAPS
AF
DET
674
DETAILED INSPECTION (DET) OF THE LH AND RH TRACK 4
DRIVE STATION ELEMENTS (DOWN DRIVE, DOWN DRIVE SHAFT,
GEARED ROTARY ACTUATOR (GEARBOX), GEARED ROTARY
ACTUATOR (OUTPUT LEVER AND FORK END), AND DRIVE
STRUT), FOLLOWED BY A GENERAL VISUAL INSPECTION (GVI)
OF THE LH AND RH TRACK 4 SENSOR STRUTS.
I:
SEMR
275400-220-805
SEMR REFERENCE:
275000-00002-1-E
1
1
0.75 A330-800
0.75 OR
A330-900
24 MO
OR
3300 FC
NOTE:
NO SHORT-TERM EXTENSION IS ALLOWED.
R
275000-15-1
212 FLAPS
AF
530
630 OPERATIONAL CHECK OF INTERCONNECTING STRUT AND
PROXIMITY SENSORS.
OPC
I: 36000 FH
MRB 8
275100-710-803
MRB REFERENCE:
27.50.00/15
PREP.: FLAPS EXTENDED;
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
1
1
1
*
REV. DATE: JUL 01/21
SECTION:
2-27
TBD ALL
TBD
TBD
0.02
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
275000-16-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
212 FLAPS
AF
530
630 OPERATIONAL CHECK OF TRACK 4 SENSOR STRUT AND
PROXIMITY SENSORS.
OPC
I: 36000 FH
SOURCE
MRB 8
REFERENCE
275400-710-803
MRB REFERENCE:
27.50.00/16
PREP.: FLAPS EXTENDED;
R
275100-01-1
148 FLAPS
AF
SVC
I:
24 MO
MRB 6
TOP UP PCU TO CONFIRM FLUID LEVEL.
ACCESS: 734
275117-01-1
275400-01-1
744
212 FLAPS
AF
500 FLAPS
AF
600
DRAIN AND REFILL ROTARY ACTUATORS AND IPGBS WITH
SEMI-FLUID.
PREP.: MOVABLE
MOVABLE
MOVABLE
MOVABLE
MOVABLE
MOVABLE
MOVABLE
MOVABLE
FLAP
FLAP
FLAP
FLAP
FLAP
FLAP
FLAP
FLAP
TRACK
TRACK
TRACK
TRACK
TRACK
TRACK
TRACK
TRACK
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FNC
I:
12 YE
MRB 8
275117-280-801
SVC
I:
72 MO
MRB 6
121327-612-804
MRB REFERENCE:
27.50.00/05
Z531;
Z532;
Z533;
Z534;
Z631;
Z632;
Z633;
Z634;
140 FLAPS
500
600 DETAILED INSPECTION OF TRANSMISSION ASSY.
AF
DET
I:
60 MO
MRB 6
275400-200-801
MRB REFERENCE:
27.50.00/03
PREP.: FLAPS EXTENDED;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
APPLICABILITY
TBD ALL
TBD
TBD
*
0.02
1
0.15 ALL
*
0.30
1
0.25 ALL
1
1
1.00 ALL
1.00
MRB REFERENCE:
27.50.00/08
27.80.00/05
ACCESS: 734
744
275400-02-1
1
1
1
M/H
MRB REFERENCE:
27.50.00/02
REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE.
R
121327-612-802
MEN
*
32.00
*
*
0.15
0.15
1
1
1
0.70 ALL
0.70
0.70
*
0.02
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
275400-02-1
ZONE
* * * * *
ACCESS: 572DB
672DB
275400-03-1
C O N T I N U E
275400-04-2
REFERENCE
MEN
M/H
*
*
0.18
0.18
1
1
1
1.00 ALL
1.00
1.00
APPLICABILITY
* * * * *
140 FLAPS
AF
DET
500
600 DETAILED INSPECTION OF CRUISE ROLLERS, FLAP TRACKS
AND CARRIAGES, ROTARY ACTUATORS AND ATTACHMENTS.
I:
60 MO
MRB 9
275400-200-802
MRB REFERENCE:
27.50.00/04
*
*
0.02
16.00
*
16.00
*
*
3.55
3.55
1
1
0.50 PRE 40701
0.50 (27-3023)
PRE 47372
PRE 51363
PREP.: FLAPS EXTENDED;
*
0.02
ACCESS: 734
744
*
*
0.15
0.15
1
1
0.50 POST 51363
0.50
ACCESS: 147AB
148AB
275400-04-1
SOURCE
734
744
PREP.: FLAPS EXTENDED;
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
R
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
147BB
148BB
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
147BT
148BT
Z531;
Z532;
Z533;
Z534;
Z631;
Z632;
Z633;
Z634;
734
744
500 FLAPS
AF
600
LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER
BEARINGS.
500 FLAPS
AF
600
LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER
BEARINGS.
LUB
LUB
I:
I:
1500 FC
OR
4000 FH
36 MO
NOTE
MRB 9
122227-640-803
MRB REFERENCE:
27.50.00/01
MRB 9
122227-640-803
MRB REFERENCE:
27.50.00/13
NOTE:
INTERVAL IS ONLY APPLICABLE WITH THE USE OF CASTROL
AEROPLEX 444 GREASE.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
275400-04-2
R
275400-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: FLAPS EXTENDED;
*
0.02
ACCESS: 734
744
*
*
0.15
0.15
1
1
1.50 ALL
1.50
*
1.52
1
1
0.15 PRE
0.15
*
0.02
1
1
0.15 POST 201497
0.15
*
0.02
1
1
0.30 PRE
0.30
PREP.: FLAPS EXTENDED;
*
0.02
ACCESS: 734
744
*
*
0.15
0.15
* * * * *
C O N T I N U E
SOURCE
REFERENCE
* * * * *
580 FLAPS
AF
680
DETAILED INSPECTION OF INTERCONNECTION STRUT AND
ATTACHMENTS.
DET
I:
72 MO
MRB 8
275100-200-801
MRB REFERENCE:
27.50.00/07
PREP.: FLAP KINK SEALS Z500;
FLAP KINK SEALS Z600;
FLAPS EXTENDED;
R
275400-06-1
147 FLAPS
AF
SVC
148
TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL.
I:
36 MO
MRB 6,9
275400-210-802
MRB REFERENCE:
27.50.00/09
PREP.: FLAPS EXTENDED;
MAIN GEAR DOORS;
N
275400-06-2
147 FLAPS
AF
SVC
148
TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL.
I:
48 MO
MRB 6
275400-210-802
275400-07-1
500 FLAPS
AF
LUB
600
LUBRICATION OF FLAP CARRIAGE (2 TO 5) LEVER BEARINGS.
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
201497
MRB REFERENCE:
27.50.00/17
PREP.: FLAPS EXTENDED;
MAIN GEAR DOORS;
R
APPLICABILITY
I:
1500 FC
OR
4000 FH
MRB 9
REV. DATE: JUL 01/21
122227-640-809
MRB REFERENCE:
27.50.00/11
SECTION:
2 -27
43303
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
275400-08-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
570 FLAPS
670
LUBRICATION OF STEADY BEARINGS.
AF
LUB
I:
24 MO
SOURCE
MRB 6
122227-640-806
MRB REFERENCE:
27.50.00/12
PREP.: FLAPS EXTENDED;
275400-11-1
REFERENCE
530 FLAPS
AF
DET
630
PERFORM A SIMULTANEOUS DETAILED VISUAL INSPECTION OF
THE INPUT GEAR BOXES (IPGB) AND OF THE DOWN DRIVE
SHAFTS (DDS) ON ALL FLAP TRACKS ON BOTH WINGS.
T:
NOTE
I:
6 YE
NOTE
SEMR
275400-220-801
MEN
M/H
APPLICABILITY
1
1
0.30 ALL
0.30
*
0.02
1
1
4.00 MSN 0001-0420
4.00 PRE 200492
PRE 201194
(27-3173)
SEMR REFERENCE:
275000-00001-2-E
NOTE:
- FIRST INSPECTION IS PERFORMED IN ACCORDANCE WITH
SB A330-27-3151. REPORT INSPECTION RESULTS, WHATEVER
THEY ARE, TO AIRBUS. SUBSEQUENT REPETITIVE INSPECTION
PERFORMED IN ACCORDANCE WITH SB A330-27-3152.
- NO SHORT-TERM EXTENSION IS ALLOWED.
- 100% THRESHOLD: 16. AUGUST 2009
PREP.: FLAPS EXTENDED;
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
FLAPS EXTENDED;
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
ACCESS: 573BB
574KB
673BB
674KB
275400-11-2
573FB
574LB
673FB
674LB
FAIRING
FAIRING
FAIRING
FAIRING
Z531;
Z532;
Z533;
Z534;
FAIRING
FAIRING
FAIRING
FAIRING
Z631;
Z632;
Z633;
Z634;
*
16.02
*
16.02
574BB
574CB
574EB
574FB
*
3.55
674BB
674CB
674EB
674FB
*
3.55
1
1
3.00 MSN 0421-9999
3.00 PRE 200492
PRE 201194
(27-3173)
530 FLAPS
AF
DET
630
PERFORM A SIMULTANEOUS DETAILED VISUAL INSPECTION OF
THE INPUT GEAR BOXES (IPGB) AND OF THE DOWN DRIVE
SHAFTS (DDS) ON ALL FLAP TRACKS ON BOTH WINGS.
T:
I:
6 YE
OR
NOTE
SEMR
275400-220-801
SEMR REFERENCE:
275000-00001-3-E
6 YE
NOTE
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 19
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
275400-11-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
16.02
*
16.02
APPLICABILITY
* * * * *
- NO SHORT-TERM EXTENSION IS ALLOWED.
- 100% THRESHOLD: 26. OCTOBER 2009, WHICHEVER OCCURS
LATER.
PREP.: FLAPS EXTENDED;
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
FLAPS EXTENDED;
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
MOVABLE FLAP TRACK
ACCESS: 573BB
574KB
673BB
674KB
275400-12-1
573FB
574LB
673FB
674LB
FAIRING
FAIRING
FAIRING
FAIRING
Z531;
Z532;
Z533;
Z534;
FAIRING
FAIRING
FAIRING
FAIRING
Z631;
Z632;
Z633;
Z634;
574BB
574CB
574EB
574FB
*
3.55
674BB
674CB
674EB
674FB
*
3.55
1
1
0.25 POST 200492
0.25 PRE 201194
(27-3173)
*
0.02
1
1
0.25 POST 201194
0.25 (27-3173)
*
0.02
1
1
1
1
0.25 ALL
0.25
0.25
0.25
530 FLAPS
AF
LUB
630
LUBRICATE THE SPLINE JOINT BETWEEN THE INPUT GEAR
BOXES (IPGB) AND THE DOWN DRIVE SHAFTS (DDS) FOR ALL
FLAP TRACKS ON BOTH WINGS.
T:
24 MO
I:
24 MO
SEMR
122227-640-817
SEMR REFERENCE:
275000-00001-4-E
PREP.: FLAPS EXTENDED;
275400-12-2
530 FLAPS
AF
LUB
630
LUBRICATE THE SPLINE JOINT BETWEEN THE INPUT GEAR
BOXES (IPGB) AND THE DOWN DRIVE SHAFTS (DDS) FOR ALL
FLAP TRACKS ON BOTH WINGS.
I:
24 MO
SEMR
122227-640-817
SEMR REFERENCE:
275000-00001-5-E
PREP.: FLAPS EXTENDED;
275400-14-1
148 FLAPS
AF
OPC
210
574 OPERATIONAL CHECK OF FLAP WTB/POB PERFORMANCE TEST.
674
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
I:
6400 FH
MRB 8
275100-710-801
MRB REFERENCE:
27.50.00/14
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 20
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
275400-14-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
275500-01-1
533 FLAPS
633
DETAILED INSPECTION OF TRACK 4 SENSORS.
AF
DET
I:
72 MO
MRB 8
275100-200-802
MRB REFERENCE:
27.50.00/06
PREP.: FLAPS EXTENDED;
276400-01-1
580 SPOILER HYDRAULIC ACTUATION
AF
LUB
680
LUBRICATION OF ALL SPOILER LINKAGE BEARINGS PROVIDED
WITH GREASE NIPPLES.
I:
18 MO
MRB 9
122227-640-805
210 SPOILER HYDRAULIC ACTUATION
AF
580
680 DETAILED INSPECTION OF LINKAGE AND ATTACHMENT OF
SPOILERS 1 TO 6.
DET
I:
4 C
MRB 9
276400-200-801
MRB REFERENCE:
27.64.00/02
PREP.: FLAPS EXTENDED;
SLATS EXTENDED;
SPOILERS EXTENDED;
R
276400-03-1
210 SPOILER HYDRAULIC ACTUATION
AF
OPC
570
670 OPERATIONAL CHECK OF SPOILER SERVOCONTROL HYDRAULIC
LOCKING FUNCTION.
I: 24000 FH
MRB 8
276400-710-802
MRB REFERENCE:
27.64.00/03
PREP.: FLAPS EXTENDED;
N
276400-03-2
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
*
*
0.05
0.05
1
1
0.10 ALL
0.10
*
0.02
1
1
1.00 ALL
1.00
*
0.15
1
1
1
0.80 ALL
0.80
0.80
*
0.27
1
1
1
0.20 A330-200
0.20 OR
0.20 A330-200F
OR
A330-300
0.02 OR
A330-900
*
210 SPOILER HYDRAULIC ACTUATION
AF
OPC
570
670 OPERATIONAL CHECK OF SPOILER SERVOCONTROL HYDRAULIC
LOCKING FUNCTION.
* * * * *
APPLICABILITY
MRB REFERENCE:
27.64.00/01
PREP.: SPOILERS EXTENDED;
276400-02-1
M/H
* * * * *
ACCESS: 574HB
674HB
R
MEN
I:
48 MO
OR
24000 FH
CMR*
MRB 8
276400-710-802
CMR REFERENCE:
276400-00001-1-C
1
1
1
0.20 A330-800
0.20
0.20
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 21
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
276400-03-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
278000-01-1
MEN
M/H
MRB REFERENCE:
27.64.00/03
*
0.02
122227-640-804
1
1
1.00 ALL
1.00
*
0.10
510 LIFT AUGMENTING (SLATS)
AF
LUB
610
LUBRICATION OF ALL SLAT TRACK ROLLER BEARINGS, PINION
BEARINGS, PINION AND RACK TEETH AND SLAT TRACK 2 AND
3 LEVER BEARINGS.
I:
1500 FC
OR
4000 FH
MRB 6,9
MRB REFERENCE:
27.80.00/01
PREP.: SLATS EXTENDED;
ACCESS: 521BB
522LB
523GB
621BB
622LB
623GB
R
278000-02-1
521DB
522NB
523JB
621DB
622NB
623JB
521GB
522RB
523LB
621GB
622RB
623LB
521JB
522TB
523NB
621JB
622TB
623NB
522CB
523CB
522JB
523EB
*
7.30
622CB
623CB
622JB
623EB
*
7.30
1
1
2.50 ALL
2.50
*
0.10
*
17.52
*
9.32
1
0.15 ALL
500 LIFT AUGMENTING (SLATS)
AF
DET
600
DETAILED INSPECTION OF SLAT TRANSMISSION ASSY, SLAT
TRACKS AND ROLLERS, PINIONS AND CURVED RACK GEARS.
I:
72 MO
MRB 6,9
MRB CPCP
R
278000-03-1
192GB
521DB
522CB
522RB
523JB
621BB
622AB
622LB
623EB
193DB
521FB
522FB
522TB
523LB
621CB
622BB
622NB
623GB
195AB
521GB
522HB
522UB
523NB
621DB
622CB
622RB
623JB
521AB
521JB
522JB
523CB
521BB
522AB
522LB
523EB
621FB
622FB
622TB
623LB
621GB
622HB
622UB
623NB
190 LIFT AUGMENTING (SLATS)
AF
SVC
I:
24 MO
MRB 6
TOP UP PCU GEARBOX TO CONFIRM FLUID LEVEL.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
278400-210-801
MRB REFERENCE:
27.80.00/03
27.80.00/04
574407-01-1
574507-01-1
574607-01-1
574707-01-1
574807-01-1
574907-01-1
PREP.: SLATS EXTENDED;
ACCESS: 191FB
521CB
522BB
522NB
523GB
621AB
621JB
622JB
623CB
APPLICABILITY
* * * * *
PREP.: FLAPS EXTENDED;
R
REFERENCE
121327-612-803
MRB REFERENCE:
27.80.00/02
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 22
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
278000-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
278000-04-1
190 LIFT AUGMENTING (SLATS)
AF
SVC
I:
36 MO
MRB 6,9
TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL.
278400-210-802
278000-04-2
N
278000-04-3
190 LIFT AUGMENTING (SLATS)
AF
SVC
I:
48 MO
MRB 6,9
278400-210-802
278000-06-1
1
0.20 PRE
*
1.00
201497
500 LIFT AUGMENTING (SLATS)
AF
LUB
600
LUBRICATION OF SLAT ROTARY ACTUATOR TYPE A (TRACK
2-3).
1
TBD POST 201497
MRB REFERENCE:
27.80.00/12
ACCESS: 193BB
R
1.80
************** TASK DELETED **************
TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL.
278000-05-1
*
APPLICABILITY
MRB REFERENCE:
27.80.00/06
ACCESS: 193BB
D
M/H
* * * * *
ACCESS: 195CB
R
MEN
I:
72 MO
MRB 6
1.00
1
1
PREP.: SLATS EXTENDED;
*
0.20 POST 50471
0.20 (27-3100)
OR
POST 50138
(27-3105)
0.10
ACCESS: 521DB
621DB
*
*
0.65
0.65
1
1
1
0.10 ALL
0.10
0.10
*
0.10
*
*
*
2.50
1.47
1.47
MRB REFERENCE:
27.80.00/07
521GB
621GB
190 LIFT AUGMENTING (SLATS)
500
600 LUBRICATION OF STEADY BEARINGS.
AF
LUB
I:
24 MO
MRB 6
522AB
622AB
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
522BB
622BB
522HB
622HB
122227-640-813
MRB REFERENCE:
27.80.00/08
PREP.: SLATS EXTENDED;
ACCESS: 193DB
521BB
621BB
122227-640-808
*
523CB
623CB
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 23
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
278000-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
520 LIFT AUGMENTING (SLATS)
AF
LUB
620
LUBRICATION OF SLAT ROTARY ACTUATOR TYPE B (TRACK
5-16).
I:
72 MO
SOURCE
MRB 6
REFERENCE
122227-640-815
278000-10-1
N
278000-11-1
522JB
523EB
622JB
623EB
522LB
523GB
622LB
623GB
522NB
523JB
622NB
623JB
522RB
523LB
622RB
623LB
522TB
523NB
622TB
623NB
210 LIFT AUGMENTING (SLATS)
AF
OPC
523
623 OPERATIONAL CHECK OF SLAT WTB/POB PERFORMANCE TEST.
I:
193 LIFT AUGMENTING (SLATS)
AF
SVC
521
621 DRAIN AND REFILL THE TEE GEARBOX AND BEVEL GEARBOXES.
I:
6400 FH
MRB 8
278100-710-801
MRB REFERENCE:
27.80.00/10
72 MO
MRB 6
MRB REFERENCE:
27.80.00/11
ACCESS: 193BB
521AB
621AB
279000-01-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
AF
OPC
I: 12000 FH
MRB 9
OPERATIONAL CHECK OF FCPCS AND FCSCS AILERON SERVO
LOOPS.
279000-02-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM
AF
OPC
210 ELECTRICAL FLIGHT CONTROL SYSTEM
AF
OPC
I: 12000 FH
MRB 9
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
1.00 ALL
1.00
*
0.10
*
6.00
*
6.00
1
1
1
0.30 ALL
0.30
0.30
1
1
1
TBD ALL
TBD
TBD
279600-710-801
*
*
*
1.00
0.40
0.40
1
0.20 ALL
279600-710-802
1
0.20 A330-200
PRE 49144
OR
A330-300
PRE 49144
1
0.20 ALL
MRB REFERENCE:
27.21.00/03
27.90.00/02
I:
800 FH
CMR**
MRB 9
OPERATIONAL CHECK OF FCPCS AND FCSCS STANDBY SERVO
* * * * *
1
1
APPLICABILITY
MRB REFERENCE:
27.14.00/06
27.90.00/06
OPERATIONAL CHECK OF FCPCS AND FCSCS YAW DAMPER SERVO
LOOPS.
279000-03-3
M/H
MRB REFERENCE:
27.80.00/09
PREP.: SLATS EXTENDED;
ACCESS: 522CB
523CB
622CB
623CB
MEN
279600-710-803
CMR REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 24
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
279000-03-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
LOOPS ON PITCH CONTROL.
279000-00001-1-C
MRB REFERENCE:
27.34.00/05
27.90.00/09
279000-04-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM
AF
OPC
I: 12000 FH
MRB 8
OPERATIONAL CHECK OF TAKEOVER AND PRIORITY FUNCTION.
279000-05-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM
AF
OPC
279600-710-804
2
0.40 ALL
1
0.50 ALL
2
0.40 ALL
2
0.40 A330-200
PRE 49144
OR
A330-300
PRE 49144
2
0.10 A330-200
POST 44047
(27-3039)
PRE 49144
OR
A330-300
POST 44047
(27-3039)
MRB REFERENCE:
27.90.00/01
I:
OPERATIONAL CHECK OF GREEN SERVOCONTROLS TRAVEL SPEED
LIMITATION WHEN RAT IS EXTENDED.
24 MO
OR
12000 FH
CMR**
MRB 8
279600-710-806
CMR REFERENCE:
279000-00002-1-C
MRB REFERENCE:
27.90.00/07
279000-06-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF FCPC1 AND FCSC1 POWER SUPPLY.
279000-08-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
AF
OPC
MRB REFERENCE:
27.90.00/04
I:
4 C
MRB 9
OPERATIONAL CHECK OF RETURN TO LOW SPEED
CONFIGURATION OF RUDDER AND PEDAL TRAVEL LIMITATION
UNITS.
279000-09-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM
EL
OPC
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
279600-710-808
MRB REFERENCE:
27.90.00/08
I:
24 MO
MRB 9
OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2.
* * * * *
279600-710-805
279600-710-819
MRB REFERENCE:
27.90.00/11
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 25
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
279000-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PRE
279000-09-2
210 ELECTRICAL FLIGHT CONTROL SYSTEM
EL
OPC
I:
OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2.
24 MO
OR
12000 FH
CMR**
MRB 9
279600-710-819
49144
2
0.10 POST 44047
(27-3039)
POST 49144
1
1
0.25 A330-200
0.25 POST 44385
(27-3040),
(27-3159)
OR
A330-300
POST 44385
(27-3040),
(27-3159)
OR
A330-200F
OR
A330-800
OR
A330-900
1
0.40 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
CMR REFERENCE:
279000-00004-1-C
MRB REFERENCE:
27.90.00/11
279000-11-1
R
279000-14-2
120 ELECTRICAL FLIGHT CONTROL SYSTEM
210
OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY.
EL
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
AV
OPC
I:
24 MO
MRB 9
MRB REFERENCE:
27.90.00/10
OPC
I:
5000 FH
MRB 8
OPERATIONAL CHECK OF THE BACK UP CONTROL MODULE AND
BACK UP POWER SUPPLY (BCM/BPS).
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
279600-710-814
279900-740-801
MRB REFERENCE:
27.90.00/14
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 26
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
279000-15-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
AV
OPC
I: 12000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP.
279000-16-1
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
AV
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
OPC
I:
5000 FH
MRB 8
210 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
EL
OPC
I:
24 MO
MRB 9
EL
OPC
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
279600-710-813
I:
24 MO
MRB 9
279600-710-820
MRB REFERENCE:
27.90.00/20
APPLICABILITY
0.40 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
1
0.40 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
A330-800
OR
A330-900
2
0.30 A330-200
POST 44047
(27-3039)
PRE 49144
OR
A330-300
POST 44047
(27-3039)
PRE 49144
1
0.30 A330-200
POST 49144
OR
A330-300
POST 49144
OR
A330-200F
OR
MRB REFERENCE:
27.90.00/19
OPERATIONAL CHECK OF PFTU-TRIM 2 NORMAL/BACK-UP POWER
SUPPLY.
* * * * *
279900-710-801
M/H
1
MRB REFERENCE:
27.90.00/16
OPERATIONAL CHECK OF POWER SUPPLY OF THE RTA2, RTLU
AND PTLU MOTOR 2.
279000-20-1
279600-710-817
MEN
MRB REFERENCE:
27.90.00/15
OPERATIONAL CHECK RUDDER ELECTRICAL BACK UP.
279000-19-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-27
PAGE 27
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
279000-20-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-800
OR
A330-900
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : FLIGHT CONTROLS
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -27
PAGE 28
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281100-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
330 TANKS
AF
SVC
340
OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER
FROM TRIM TANK AND TRIM VENT SURGE TANK.
I:
2 MO
NOTE
SOURCE
CMP
MRB 9
1
0.15 ALL
1
0.05 ALL
2
2
0.15 ALL
0.15
PREP.: FUEL TANK DRAINED AND VENTED;
*
2.00
ACCESS: 541BB
641BB
*
*
0.50
0.50
1
1
0.60 A330-200F
0.60 POST 58623
PRE 200281
OR
A330-300
PRE 204025
AF
OPC
MRB REFERENCE:
28.11.00/02
28.42.00/03
I:
24 MO
MRB 9
210 TANKS
AF
OPC
281100-07-1
281100-08-1
540 TANKS
AF
OPC
640
OPERATIONAL CHECK OF STANDBY FUEL CELL CLACK VALVES
TO ENSURE FULL AND FREE MOVEMENT.
500 TANKS
AF
SVC
600
OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER
FROM INNER, OUTER AND WING VENT SURGE TANKS.
I:
6 YE
MRB 8
SYSTEMS, APU AND POWER PLANT : FUEL
281100-710-802
MRB REFERENCE:
28.11.00/04
I:
144 MO
MRB 9
281100-710-805
MRB REFERENCE:
28.11.00/08
I:
10 DY
NOTE
CMP
MRB 9
123228-281-806
CMP REFERENCE:
28-2-0000-011
NOTE:
* * * * *
281100-710-801
MRB REFERENCE:
28.11.00/03
OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE
TO PROVE THAT NEITHER VALVE HAS JAMMED IN THE OPEN
POSITION AND TO VERIFY CORRECT OPERATION OF THE
P/BSW.
R
APPLICABILITY
CMP REFERENCE:
28-2-0000-010
OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE,
USING INDIVIDUAL MOTORS, TO PROVE CORRECT ACTUATOR
OPERATION AND COCKPIT INDICATION.
281100-06-1
M/H
0.15 ALL
0.15
210 TANKS
123228-281-803
MEN
1
1
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
281100-05-1
REFERENCE
MRB REFERENCE:
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281100-08-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
281100-09-1
281100-10-1
M/H
APPLICABILITY
540 TANKS
AF
OPC
640
OPERATIONAL CHECK OF ALL COLLECTOR CELL CLACK VALVES
TO ENSURE FULL AND FREE MOVEMENT.
28.11.00/01
28.42.00/01
2
2
0.15 ALL
0.15
PREP.: FUEL TANK DRAINED AND VENTED;
*
2.00
ACCESS: 541AB
641AB
*
*
0.50
0.50
1
1
1
0.50 A330-200
0.50 OR
0.50 A330-200F
PRE 58623
OR
A330-200F
POST 200281
OR
A330-300
POST 204025
OR
A330-800
0.02 OR
A330-900
POST 204025
190 TANKS
AF
SVC
500
600 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER
FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS.
I:
144 MO
MRB 9
ACCESS: 191RB
281100-710-806
MRB REFERENCE:
28.11.00/05
I:
10 DY
NOTE
CMP
MRB 9
123228-281-810
CMP REFERENCE:
28-2-0000-013
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
281200-02-1
MEN
* * * * *
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
R
REFERENCE
MRB REFERENCE:
28.11.00/09
28.42.00/02
192RB
*
346 TANK VENTING SYSTEM
AF
VCK
550
650 VISUAL CHECK OF THE WING AND TRIM VENT SURGE TANK
OVERPRESSURE PROTECTORS (BURST DISCS) FOR INTEGRITY.
I:
24 MO
NOTE
MRB 9
281200-210-802
MRB REFERENCE:
28.12.00/02
1
1
1
0.05 ALL
0.05
0.05
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281200-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
281300-01-1
190 CENTER BOX VENTING AND DRAINAGE
AF
OPC
I:
1000 FH
MRB 9
OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING
CENTER BOX.
281800-01-1
140 IGNITION PREVENTION
AF
DET
300
500 DETAILED INSPECTION OF THE WING AND TRIM TANK BONDING
600 LEADS (SFAR88).
PREP.: FIXED
FIXED
FIXED
FIXED
FIXED
FIXED
ACCESS: 147AZ
319AL
333CB
343BB
541AB
541DB
541GB
541MB
542AB
542GB
550CB
641AB
641DB
641GB
641MB
642AB
642GB
650CB
SYSTEMS, APU AND POWER PLANT : FUEL
FLAP
FLAP
FLAP
FLAP
FLAP
FLAP
TRACK
TRACK
TRACK
TRACK
TRACK
TRACK
148AZ
319AR
333DB
343CB
541AZ
541DZ
541GZ
541NB
542BB
542HB
550DB
641AZ
641DZ
641GZ
641NB
642BB
642HB
650DB
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
319BL
333EB
343DB
541BB
541EB
541HB
541PB
542CB
542JB
550EB
641BB
641EB
641HB
641PB
642CB
642JB
650EB
I:
144 MO
MRB 9
281800-200-801
MRB REFERENCE:
28.18.00/01
Z532;
Z533;
Z534;
Z632;
Z633;
Z634;
319DR
333FB
343EB
541BZ
541EZ
541JB
541QB
542DB
542KB
550FB
641BZ
641EZ
641JB
641QB
642DB
642KB
650FB
333AL
333GB
343FB
541CB
541FB
541KB
541RB
542EB
550AB
333BB
343AR
343GB
541CZ
541FZ
541LB
541SB
542FB
550BB
641CB
641FB
641KB
641RB
642EB
650AB
641CZ
641FZ
641LB
641SB
642FB
650BB
1
0.05 A330-200F
POST 58623
PRE 200281
OR
A330-300
PRE 204025
2
2
2
2
2.50 ALL
2.50
2.50
2.50
*
6.00
*
6.50
*
*
0.80
16.20
*
27.65
*
27.65
MRB REFERENCE:
28.13.00/01
28.22.00/06
28.23.00/03
28.25.00/03
NOTE:
ETOPS RELEVANT
R
281300-710-801
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
281800-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
190 IGNITION PREVENTION
AF
DET
I:
6 YE
SOURCE
FAL
MRB 8
DETAILED INSPECTION OF THE HEATSHIELDS BELOW THE
CENTER TANK (SFAR88).
ACCESS: 192PB
R
R
281800-03-1
281800-04-1
REFERENCE
281852-210-801
MEN
1
FAL REFERENCE:
281800-00002-1-F
193DB
M/H
0.60 A330-200
POST 49520
(21-3096)
OR
A330-200F
4.50 PRE 58623
OR
A330-200F
POST 200281
OR
A330-300
POST 204025
OR
A330-800
OR
A330-900
MRB REFERENCE:
28.18.00/04
*
281851-210-801
2
2
2
2
0.50 ALL
0.50
0.50
0.50
PREP.: FUEL TANK DRAINED AND VENTED;
*
2.00
ACCESS: 147AZ
312AR
541AB
641AB
*
*
*
*
0.80
3.01
1.00
1.00
2
2
2
2
2.50 ALL
2.50
2.50
2.50
*
6.00
*
6.50
*
*
0.80
16.20
140 IGNITION PREVENTION
AF
300
500 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS
600 (SFAR88).
148AZ
319DR
541BB
641BB
GVI
ACCESS: 147AZ
319AL
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
FLAP
FLAP
FLAP
FLAP
FLAP
FLAP
TRACK
TRACK
TRACK
TRACK
TRACK
TRACK
148AZ
319AR
144 MO
MRB 9
MRB REFERENCE:
28.18.00/03
319ER
140 IGNITION PREVENTION
AF
GVI
300
500 GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND
600 PROBE ATTACHMENTS (SFAR88).
PREP.: FIXED
FIXED
FIXED
FIXED
FIXED
FIXED
I:
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
319BL
144 MO
MRB 9
281844-210-801
MRB REFERENCE:
28.18.00/02
Z532;
Z533;
Z534;
Z632;
Z633;
Z634;
319DR
C O N T I N U E D
I:
333AL
333BB
APPLICABILITY
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-28
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281800-04-1
ZONE
* * * * *
333CB
343BB
541AB
541DB
541GB
541MB
542AB
542GB
550CB
641AB
641DB
641GB
641MB
642AB
642GB
650CB
281800-05-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
333DB
343CB
541AZ
541DZ
541GZ
541NB
542BB
542HB
550DB
641AZ
641DZ
641GZ
641NB
642BB
642HB
650DB
333EB
343DB
541BB
541EB
541HB
541PB
542CB
542JB
550EB
641BB
641EB
641HB
641PB
642CB
642JB
650EB
SOURCE
333FB
343EB
541BZ
541EZ
541JB
541QB
542DB
542KB
550FB
641BZ
641EZ
641JB
641QB
642DB
642KB
650FB
333GB
343FB
541CB
541FB
541KB
541RB
542EB
550AB
343AR
343GB
541CZ
541FZ
541LB
541SB
542FB
550BB
641CB
641FB
641KB
641RB
642EB
650AB
641CZ
641FZ
641LB
641SB
642FB
650BB
AF
VCK
I:
700 FH
MRB 8
VISUAL CHECK OF CENTER TANK FOR LEAKS (SFAR88).
281800-06-1
AF
GVI
I:
72 MO
MRB 9
GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD
CARGO BAY INSULATION MATS (SFAR88).
SYSTEMS, APU AND POWER PLANT : FUEL
131CX
131DX
132CX
281852-210-803
MRB REFERENCE:
28.18.00/05
192RB
130 IGNITION PREVENTION
ACCESS: 131BX
MEN
M/H
*
27.65
*
27.65
APPLICABILITY
* * * * *
190 IGNITION PREVENTION
ACCESS: 191RB
REFERENCE
281852-210-802
1
0.30 A330-200
PRE 49520
(21-3096)
*
0.02
1
0.30 A330-200
OR
A330-200F
PRE 58623
OR
0.75 A330-200F
POST 200281
OR
A330-300
POST 204025
OR
A330-800
OR
A330-900
POST 204025
MRB REFERENCE:
28.18.00/06
132DX
*
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
281800-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
250 IGNITION PREVENTION
AF
GVI
I:
144 MO
SOURCE
MRB 9
GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE
CENTER TANK (SFAR88).
REFERENCE
281842-210-801
281800-08-1
*
500 IGNITION PREVENTION
AF
GVI
600
GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND
TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS
(SFAR88).
I:
144 MO
MRB 9
281841-210-801
R
281800-09-1
1.00 ALL
1.00
*
0.12
521DB
522BB
522JB
523EB
573DB
575BB
521FB
522BT
522LB
523GB
573FB
575BT
521GB
522CB
522NB
523JB
573GB
575CB
*
14.22
621BB
622AB
622EB
622UB
623NB
675AB
621CB
622AT
622HB
623CB
673CB
675AT
621DB
622BB
622JB
623EB
673DB
675BB
621FB
622BT
622LB
623GB
673FB
675BT
621GB
622CB
622NB
623JB
673GB
675CB
*
14.22
GVI
I:
144 MO
MRB 9
GENERAL VISUAL INSPECTION OF TRIM TANK EXTERNAL
SYSTEMS, APU AND POWER PLANT : FUEL
1
1
521CB
522AT
522HB
523CB
573CB
575AT
AF
C O N T I N U E D
APPLICABILITY
0.50 A330-200
OR
A330-200F
PRE 58623
OR
98.00 A330-200F
POST 200281
OR
A330-300
POST 204025
OR
A330-800
OR
A330-900
POST 204025
521BB
522AB
522EB
522UB
523NB
575AB
300 IGNITION PREVENTION
* * * * *
M/H
MRB REFERENCE:
28.18.00/08
PREP.: FLAPS EXTENDED;
SLATS EXTENDED;
ACCESS: 521AB
521JB
522CT
522TB
523LB
574AT
575DB
621AB
621JB
622CT
622TB
623LB
674AT
675DB
1
MRB REFERENCE:
28.18.00/07
PREP.: FLOOR PANELS Z250;
SEATS Z250;
R
MEN
281841-210-802
1
0.60 ALL
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281800-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
R
281800-10-1
331BT
334AB
334DB
335AB
341AT
343AT
344CT
344GB
345FB
331CT
334AT
334DT
335BB
341BT
344AB
344DB
345AB
281800-12-1
331DT
334BB
334EB
335CB
341CT
344AT
344DT
345BB
331ET
334BT
334ET
335DB
341DT
344BB
344EB
345CB
333AB
334CB
334FB
335EB
341ET
344BT
344ET
345DB
500 IGNITION PREVENTION
AF
600
GENERAL VISUAL INSPECTION OF WING FUEL PUMP
ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL
SUPPLY CABLE (SFAR88).
GVI
120 IGNITION PREVENTION
AF
OPC
210
OPERATIONAL CHECK OF CENTER TANK FUEL PUMP GROUND
FAULT INTERRUPTER (GFI)(SFAR88).
I:
144 MO
MRB 9
281843-210-801
MRB REFERENCE:
28.18.00/10
I:
24 MO
OR
4000 FH
FAL
MRB 8
281800-710-801
FAL REFERENCE:
281800-00001-1-F
MRB REFERENCE:
28.18.00/11
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
M/H
*
65.10
APPLICABILITY
28.18.00/09
PREP.: FUEL PUMP FAIRINGS Z500;
FUEL PUMP FAIRINGS Z600;
R
MEN
* * * * *
ELECTRICAL WIRING AND CONNECTIONS (SFAR88).
ACCESS: 331AT
333AT
334CT
334GB
335FB
343AB
344CB
344FB
345EB
REFERENCE
C O N T I N U E D
1
1
0.10 ALL
0.10
*
*
0.40
0.40
1
1
0.10 FAA
0.10 A330-200
POST 200242
(28-3113)
OR
FAA
A330-200F
POST 200242
(28-3113)
OR
FAA
A330-300
POST 200242
(28-3113)
OR
FAA
A330-800
OR
FAA
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
281800-12-1
281800-12-2
282100-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
120 IGNITION PREVENTION
AF
OPC
210
OPERATIONAL CHECK OF CENTER TANK FUEL PUMP GROUND
FAULT INTERRUPTER (GFI)(SFAR88).
I:
210 MAIN FUEL PUMP SYSTEM
I: 24000 FH
210 MAIN FUEL PUMP SYSTEM
MEN
M/H
APPLICABILITY
* * * * *
AF
OPC
24 MO
MRB 8
EL
OPC
281800-710-801
1
1
0.10 NON-FAA
0.10 A330-200
POST 200242
(28-3113)
OR
NON-FAA
A330-200F
POST 200242
(28-3113)
OR
NON-FAA
A330-300
POST 200242
(28-3113)
OR
NON-FAA
A330-800
POST 200242
(28-3113)
OR
NON-FAA
A330-900
POST 200242
(28-3113)
1
0.10 ALL
1
0.20 ALL
MRB REFERENCE:
28.18.00/11
MRB 8
OPERATIONAL CHECK TO VERIFY THAT RELAY 27QA HAS NOT
FAILED IN THE ENERGISED POSITION.
282100-03-1
REFERENCE
282100-710-804
MRB REFERENCE:
28.21.00/02
I:
4000 FH
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY THAT THE LEFT NO 2 PUMP
OFF FUNCTION IS OPERATIVE.
282100-710-805
CMR REFERENCE:
282100-00001-1-C
MRB REFERENCE:
28.21.00/01
SYSTEMS, APU AND POWER PLANT : FUEL
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 MAIN FUEL PUMP SYSTEM
EL
OPC
I:
4000 FH
SOURCE
CMR**
MRB 8
OPERATIONAL CHECK TO VERIFY ISOLATION OF RIGHT PUMP 2
CONTROL WHEN LEFT MAIN PUMP 2 IS RUNNING IN
ELECTRICAL EMERGENCY CONFIGURATION.
REFERENCE
282100-710-806
MEN
M/H
APPLICABILITY
1
0.20 ALL
1
0.50 ALL
1
0.20 ALL
1
1
1
0.20 PRE 44603
0.20 (28-3041)
0.20
1
0.20 NON-ETOPS
POST 42890
(28-3014)
OR
NON-ETOPS
POST 42921
(53-3016)
*
0.01
CMR REFERENCE:
282100-00001-1-C
MRB REFERENCE:
28.21.00/01
282100-06-1
210 MAIN FUEL PUMP SYSTEM
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF STANDBY PUMP AUTOMATIC CONTROL.
282100-710-812
MRB REFERENCE:
28.21.00/03
NOTE:
ETOPS RELEVANT
282100-10-1
210 MAIN FUEL PUMP SYSTEM
AF
OPC
I:
24 MO
MRB 8
OPERATIONAL CHECK TO ENSURE THAT THE RIGHT NO.2 MAIN
FUEL PUMP OPERATES WHEN THE LEFT NO.2 MAIN FUEL PUMP
IS SWITCHED OFF IN ELECTRICAL EMERGENCY
CONFIGURATION.
282200-06-2
211 APU FUEL PUMP SYSTEM
AF
OPC
212
311 OPERATIONAL CHECK OF FWD APU FUEL FEED PUMP
ACTIVATION CIRCUIT VIA LANDING GEAR LGCIU1 (5GA1),
RELAY 12QC AND MAIN BOOSTER PUMP CONTACTORS (60QA1,
60QA2, 61QA1, 61QA2).
282100-710-814
MRB REFERENCE:
28.21.00/05
I:
24 MO
MRB 9
282200-710-811
MRB REFERENCE:
28.22.00/03
NOTE:
ETOPS RELEVANT
282200-07-3
311 APU FUEL PUMP SYSTEM
AF
OPC
I:
4000 FH
MRB 9
OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO
DRAIN ANY ACCUMULATED WATER.
123228-281-807
MRB REFERENCE:
28.22.00/07
NOTE:
ETOPS RELEVANT
ACCESS: 311AL
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282200-07-3
R
282200-07-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
311 APU FUEL PUMP SYSTEM
AF
OPC
I:
1000 FH
CMP
MRB 9
123228-281-807
OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO
DRAIN ANY ACCUMULATED WATER.
CMP REFERENCE:
28-2-0000-008
NOTE:
ETOPS RELEVANT
MRB REFERENCE:
28.22.00/07
147 APU FUEL PUMP SYSTEM
210
312 OPERATIONAL CHECK OF RELAYS 12QC AND 14QC
EL
OPC
I:
4600 FH
CMP
282200-710-808
CMP REFERENCE:
28-2-0000-012
ACCESS: 312AR
734
744
282200-12-1
210 APU FUEL PUMP SYSTEM
M/H
APPLICABILITY
* * * * *
ACCESS: 311AL
282200-08-1
MEN
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF AFT APU FUEL PUMP FIRE STOP
CIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS (5WF AND
6WF).
282200-710-812
1
0.20 ETOPS
*
0.01
2
2
2
0.10 ETOPS
0.10
0.10
*
*
*
0.01
0.15
0.15
1
0.20 ALL
1
0.10 ALL
MRB REFERENCE:
28.22.00/04
NOTE:
ETOPS RELEVANT
R
282300-02-1
210 CROSSFEED SYSTEM
EL
OPC
I:
48 MO
CMP
MRB 9
282300-710-803
OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL
MOTORS.
CMP REFERENCE:
28-2-0000-001
NOTE:
ETOPS RELEVANT
MRB REFERENCE:
28.23.00/02
SYSTEMS, APU AND POWER PLANT : FUEL
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282300-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 CROSSFEED SYSTEM
AF
OPC
OPERATIONAL CHECK OF CROSSFEED VALVE TO VERIFY THAT
INDIVIDUAL ENGINE FUEL FEED SYSTEMS CAN BE
INTERCONNECTED.
SOURCE
I: 36000 FH
OR
12 YE
MRB 8
I:
MRB 8
REFERENCE
282300-710-804
MEN
M/H
1
0.25 ALL
1
1
1
0.30 RR
0.30
0.30
*
*
0.15
0.15
2
2
0.20 ALL
0.20
1
1
1
0.40 GE
0.40
0.40
MRB REFERENCE:
28.24.00/03
*
*
0.10
0.10
282400-710-808
1
1
1
0.50 PW
0.50
0.50
*
*
0.07
0.07
APPLICABILITY
MRB REFERENCE:
28.23.00/01
NOTE:
ETOPS RELEVANT
282400-03-1
210 ENGINE LP FUEL SHUT-OFF
AF
OPC
410
420 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL
SUPPLY TO ASSOCIATED ENGINE.
ACCESS: 415AL
425AL
282400-04-1
282400-05-1
435AL
445AL
I:
210 ENGINE LP FUEL SHUT-OFF
AF
OPC
410
420 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL
SUPPLY TO ASSOCIATED ENGINE.
I:
SYSTEMS, APU AND POWER PLANT : FUEL
MRB REFERENCE:
28.24.00/03
48 MO
MRB 9
418AR
428AR
282400-710-803
MRB REFERENCE:
28.24.00/01
12 YE
OR
6500 FC
OR
29000 FH
CMR**
MRB 8
I:
12 YE
OR
6500 FC
OR
29000 FH
282400-710-808
CMR REFERENCE:
282400-G0001-1-C
418AR
428AR
210 ENGINE LP FUEL SHUT-OFF
AF
OPC
410
420 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL
SUPPLY TO ASSOCIATED ENGINE.
ACCESS: 416BR
426BR
282400-710-807
436AR
446AR
520 ENGINE LP FUEL SHUT-OFF
EL
OPC
620
OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL
MOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT AND
CORRECT COCKPIT INDICATION.
ACCESS: 416AR
426AR
282400-06-1
416AR
426AR
12 YE
OR
6500 FC
CMR**
MRB 8
REV. DATE: JUL 01/21
CMR REFERENCE:
282400-P0001-1-C
MRB REFERENCE:
28.24.00/03
SECTION:
2-28
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282500-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
620 REFUEL/DEFUEL SYSTEM
AF
DET
I:
DETAILED INSPECTION OF REFUEL COUPLING(S) FOR DAMAGE
OR EVIDENCE OF WEAR.
48 MO
OR
4400 FC
SOURCE
MRB 9
REFERENCE
282500-220-801
520 REFUEL/DEFUEL SYSTEM
AF
DET
620
DETAILED INSPECTION OF REFUEL COUPLING(S) FOR DAMAGE
OR EVIDENCE OF WEAR.
I:
48 MO
OR
4400 FC
MRB 9
282500-220-801
210 REFUEL/DEFUEL SYSTEM
EL
OPC
OPERATIONAL CHECK TO PROVE THAT THERE IS NO FUEL
TRANSFER FROM AFT TO FWD INNER TANK WHEN EMERGENCY
ISOLATION VALVE IS SELECTED CLOSED.
R
282600-04-1
210 MAIN TRANSFER SYSTEM
AF
OPC
I: 36000 FH
OR
12 YE
MRB 8
1
0.20 PRE 40176
(28-3018)
*
0.02
1
1
0.20 POST 40176
0.20 (28-3018)
*
*
0.02
0.02
I: 82700 FH
CMR*
282500-710-802
1
0.10 ALL
1
0.30 A330-200
POST 49144
OR
A330-200
POST 200103
(00-3068)
OR
A330-200F
PRE 58623
OR
A330-200F
POST 200281
OR
A330-300
POST 204025
OR
A330-800
OR
A330-900
MRB REFERENCE:
28.25.00/02
OPERATIONAL CHECK OF MANUAL OVERRIDE PB/SW AND AND
ASSOCIATED CIRCUITRY.
SYSTEMS, APU AND POWER PLANT : FUEL
APPLICABILITY
MRB REFERENCE:
28.25.00/01
ACCESS: 522HB
622HB
282500-02-1
M/H
MRB REFERENCE:
28.25.00/01
ACCESS: 622HB
282500-01-3
MEN
282600-710-810
CMR REFERENCE:
282600-00001-1-C
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282700-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 TRIM TANK TRANSFER SYSTEM
AF
OPC
I:
48 MO
SOURCE
MRB 9
OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES
FOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH.
R
282700-02-4
210 TRIM TANK TRANSFER SYSTEM
AF
OPC
OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES
FOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH.
REFERENCE
282700-710-801
I:
48 MO
OR
25000 FH
CMR**
MRB 9
282700-710-801
CMR REFERENCE:
282700-00001-3-C
SYSTEMS, APU AND POWER PLANT : FUEL
C O N T I N U E D
M/H
APPLICABILITY
1
0.25 A330-200
PRE 45649
(28-3056)
PRE 49144
PRE 58269
PRE 200103
(00-3068)
OR
A330-300
PRE 45649
(28-3056)
PRE 49144
PRE 58269
PRE 200103
(00-3068)
1
0.25 A330-200
PRE 45649
(28-3056)
POST 49144
OR
A330-200
PRE 45649
(28-3056)
POST 58269
OR
A330-200
PRE 45649
(28-3056)
POST 200103
(00-3068)
OR
A330-200
POST 45649
(28-3056)
OR
A330-300
PRE 45649
(28-3056)
POST 49144
OR
A330-300
PRE 45649
(28-3056)
MRB REFERENCE:
28.27.00/01
MRB REFERENCE:
28.27.00/01
* * * * *
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
282700-02-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 58269
OR
A330-300
PRE 45649
(28-3056)
POST 200103
(00-3068)
OR
A330-300
POST 45649
(28-3056)
OR
A330-200F
OR
A330-800
OR
A330-900
282700-05-1
100 TRIM TANK TRANSFER SYSTEM
AF
FNC
210
310 FUNCTIONAL CHECK OF TRIM TANK TRANSFER LINE SHROUD
CONNECTORS.
ACCESS: 312AR
R
283100-01-1
I:
48 MO
OR
28000 FH
CMR**
MRB 8
AF
OPC
I:
72 MO
MRB 9
OPERATIONAL CHECK TO VERIFY CORRECT RESPONSE OF
JETTISON VALVES TO SELECTION OF JETTISON "ON".
R
283100-02-1
500 JETTISON SYSTEM
600
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
C O N T I N U E D
AF
1
1
1
0.40 ALL
0.40
0.40
MRB REFERENCE:
28.14.00/03
28.27.00/03
*
0.03
283100-710-801
1
0.15 A330-200
POST 45008
(28-3084)
OR
A330-200F
POST 45008
(28-3084)
OR
A330-800
POST 206807
1
1
0.20 A330-200
0.20 POST 45008
CMR REFERENCE:
282700-00002-1-C
313AL
210 JETTISON SYSTEM
282700-790-801
MRB REFERENCE:
28.31.00/03
GVI
I:
48 MO
MRB 9
283100-210-801
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-28
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
283100-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
283100-03-1
284600-02-1
MEN
M/H
APPLICABILITY
* * * * *
GENERAL VISUAL INSPECTION OF JETTISON PIPE FLEXIBLE
HOSE FOR SECURITY AND CONDITION.
R
REFERENCE
MRB REFERENCE:
28.31.00/01
PREP.: FLAPS EXTENDED;
*
ACCESS: 533DB
633DB
*
*
533 JETTISON SYSTEM
AF
GVI
633
GENERAL VISUAL INSPECTION OF ANTI-CORONA DEVICE FOR
SECURITY OF ATTACHMENT AND FOR SATISFACTORY
CONDITION.
I:
210 TANK LEVEL SENSING
I: 12000 FH
EL
OPC
48 MO
MRB 9
283100-210-804
MRB REFERENCE:
28.31.00/02
MRB 8
OPERATIONAL CHECK OF INNER TANK LOW LEVEL SENSORS AND
ASSOCIATED WARNINGS.
284600-710-802
(28-3084)
OR
A330-200F
0.02 POST 45008
(28-3084)
0.04 OR
0.04 A330-800
POST 206807
1
1
0.10 A330-200
0.10 POST 45008
(28-3084)
OR
A330-200F
POST 45008
(28-3084)
OR
A330-800
POST 206807
1
0.15 ALL
MRB REFERENCE:
28.46.00/02
NOTE:
ETOPS RELEVANT
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL
E N D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -28
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
D
291000-01-1
291000-02-1
ZONE
SOURCE
147 MAIN HYDRAULIC POWER
190
HYDRAULIC FLUID ANALYSIS.
AF
FNC
I:
36 MO
MRB 9
291000-05-1
123229-281-801
MRB REFERENCE:
29.10.00/11
744
210 MAIN HYDRAULIC POWER
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF EDP DEPRESSURIZATION.
291000-04-1
REFERENCE
MEN
M/H
APPLICABILITY
************** TASK DELETED **************
ACCESS: 734
291000-03-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
291000-710-802
1
1
0.20 ALL
0.20
*
0.30
1
0.30 ALL
1
1
0.60 ALL
0.60
1
0.10 ALL
*
0.30
1
1
0.10 ALL
0.10
*
0.03
1
1
1
0.10 ALL
0.10
0.10
MRB REFERENCE:
29.10.00/05
120 MAIN HYDRAULIC POWER
AV
OPC
210
OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT-OFF VALVES.
I:
190 MAIN HYDRAULIC POWER
I:
AF
DET
24 MO
MRB 8
291000-710-804
MRB REFERENCE:
29.10.00/09
24 MO
MRB 6
CHECK FOR CORRECT AIR PRESSURE BY READING GAUGES ON
EACH RESERVOIR.
291400-200-802
MRB REFERENCE:
29.10.00/06
NOTE:
ETOPS RELEVANT
ACCESS: 734
291000-06-1
147 MAIN HYDRAULIC POWER
AF
FNC
190
CHECK NITROGEN CHARGING PRESSURE ON HYDRAULIC POWER
ACCUMULATORS.
ACCESS: 195BB
291000-07-1
744
196BB
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : HYDRAULIC POWER
400 FH
MRB 9
291000-200-802
MRB REFERENCE:
29.10.00/01
197CB
147 MAIN HYDRAULIC POWER
AF
VCK
197
400 VISUAL CHECK OF CLOGGING INDICATORS OF HIGH PRESSURE
(HP), RETURN, ENGINE DRIVEN PUMPS (EDP) CASE DRAIN,
* * * * *
I:
I:
1000 FH
MRB 9
291000-200-803
MRB REFERENCE:
29.10.00/02
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-29
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
291000-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
*
0.30
0.01
0.20
1
0.10 PUA P/N 4020Q8-2
INSTALLED
OR
PUA P/N 4020Q8-3
0.30 INSTALLED
* * * * *
RESERVOIR FILL AND AIR PRESSURIZATION UNIT (PUA)
FILTERS.
ACCESS: 734 744
197CB
415AL 417AL
R
291000-08-1
425AL
427AL
195 MAIN HYDRAULIC POWER
AF
SVC
I:
1000 FH
MRB 9
DRAINING OF WATER SEPARATORS.
ACCESS: 734
291000-11-1
MRB REFERENCE:
29.10.00/03
744
195 MAIN HYDRAULIC POWER
AF
VCK
I:
3200 FH
MRB 9
VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN
VALVE POSITION.
R
291000-23-1
410 MAIN HYDRAULIC POWER
420
INSPECTION OF HYDRAULIC PULSATION DAMPER.
ACCESS: 415AL
425AL
291000-25-1
291000-26-1
AF
DET
I:
121 MAIN HYDRAULIC POWER
AF
FNC
122
210 FUNCTIONAL CHECK OF UNCONTAINED ENGINE ROTOR FAILURE
410 PROTECTION.
420
I:
195 MAIN HYDRAULIC POWER
I:
AF
VCK
291400-200-803
*
1
0.10 PUA P/N 4020Q10-2
INSTALLED
VSB
RB211-29-F577
VSB
RB211-73-AJ366
1
1
0.40 TRENT 700
0.40 PRE SB RB 73-AJ366
*
*
0.10
0.10
291000-720-803
1
1
1
1
1
0.10 A330-800
0.10 OR
0.10 A330-900
0.10
0.10
1
0.10 A330-800
OR
A330-900
MRB REFERENCE:
29.10.00/21
1000 FH
VSB
416AR
426AR
72 MO
MRB 8
MRB REFERENCE:
29.10.00/25
4000 FH
MRB 9
VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN
VALVE POSITION.
SYSTEMS, APU AND POWER PLANT : HYDRAULIC POWER
291400-600-801
291400-200-804
MRB REFERENCE:
29.10.00/26
REV. DATE: JUL 01/21
SECTION:
2 -29
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
291100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 MAIN HYDRAULIC POWER
AF
FNC
I:
72 MO
SOURCE
MRB 6,9
FUNCTIONAL CHECK OF PRIORITY VALVE.
ACCESS: 734
291100-03-1
AF
OPC
I:
24 MO
MRB 8
OPERATIONAL CHECK OF AUTOMATIC CONTROL OF FIRE
SHUT-OFF VALVE IN CASE OF LOW LEVEL ON GREEN
HYDRAULIC SYSTEM.
ACCESS: 734
291100-05-1
291100-720-801
MRB REFERENCE:
29.10.00/07
744
210 MAIN HYDRAULIC POWER
REFERENCE
291100-710-804
AF
FNC
I:
6 YE
MRB 8
REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK.
291146-750-801
500 MAIN HYDRAULIC POWER
AF
600
REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK.
FNC
I:
6 YE
MRB 8
291700-01-1
147 MAIN HYDRAULIC POWER
195
196 SERVICING OF LEAKAGE RECOVERY TANKS.
AF
291148-750-801
MRB REFERENCE:
29.10.00/18
ACCESS: 575BB
675BB
R
SVC
I:
2000 FH
MRB 9
122429-600-801
MRB REFERENCE:
29.10.00/04
ACCESS: 734
744
291900-01-1
210 HYD GROUND INTERNAL LEAK TEST SYSTEM
AF
OPC
I:
72 MO
MRB 9
OPERATIONAL CHECK OF INHIBITION OF MANUAL CONTROL OF
LEAK MEASUREMENT SOLENOID VALVE.
SYSTEMS, APU AND POWER PLANT : HYDRAULIC POWER
APPLICABILITY
2
0.30 ALL
*
0.30
2
0.30 ALL
*
0.30
1
0.50 POST 40838
*
0.01
1
1
0.40 POST 40838
0.40
*
*
0.80
0.80
1
1
1
0.05 ALL
0.05
0.05
*
*
0.15
0.15
1
0.40 ALL
MRB REFERENCE:
29.10.00/16
ACCESS: 312AR
291100-06-1
M/H
MRB REFERENCE:
29.10.00/10
744
310 MAIN HYDRAULIC POWER
MEN
291900-710-801
MRB REFERENCE:
29.10.00/14
REV. DATE: JUL 01/21
SECTION:
2-29
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
292000-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AUXILIARY HYDRAULIC POWER
AF
OPC
I:
4000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF GREEN, YELLOW AND BLUE ELECTRIC
PUMPS.
292000-02-1
R
292000-04-1
292000-05-1
I:
147 AUXILIARY HYDRAULIC POWER
AF
FNC
210
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF
GREEN HYDRAULIC SYSTEM.
I: 12000 FH
210 AUXILIARY HYDRAULIC POWER
I: 12000 FH
FNC
8000 FH
MRB 9
120 AUXILIARY HYDRAULIC POWER
AV
OPC
210
OPERATIONAL CHECK OF THE AUTOMATIC START OF THE BLUE
ELECTRIC PUMP.
292000-710-801
MRB 8
291900-720-802
MRB REFERENCE:
29.20.00/08
MRB 8
293100-720-804
120 AUXILIARY HYDRAULIC POWER
AF
140
210 OPERATIONAL CHECK OF RAM AIR TURBINE AUTOMATIC
633 DEPLOYMENT.
DETAILED INSPECTION OF THE RAM AIR TURBINE ONCE
EXTENDED.
OPC
I:
24 MO
MRB 9
292000-710-804
MRB REFERENCE:
29.20.00/10
I:
24 MO
MRB 8
292400-710-804
MRB REFERENCE:
29.20.00/03
29.20.00/05
ACCESS: 633HB
SYSTEMS, APU AND POWER PLANT : HYDRAULIC POWER
APPLICABILITY
1
0.40 ALL
1
1
1.00 ALL
1.00
1
1
0.50 ALL
0.50
2
0.50 ALL
1
1
0.25 POST 49748
0.25
*
0.22
1
1
1
1
0.75 ALL
0.75
0.75
0.75
*
0.10
MRB REFERENCE:
29.10.00/13
29.20.00/07
PREP.: FLAPS EXTENDED;
PROTECTIVE COVER ON 802VU;
SLATS EXTENDED;
292400-01-1
M/H
MRB REFERENCE:
29.20.00/02
FUNCTIONAL CHECK OF GREEN, BLUE AND YELLOW LOW LEVEL
WARNING SYSTEM.
292000-06-1
292000-710-802
MEN
MRB REFERENCE:
29.20.00/01
120 AUXILIARY HYDRAULIC POWER
AF
OPC
210
OPERATIONAL CHECK OF AUTOMATIC START OF GREEN AND
YELLOW ELECTRIC PUMPS.
AF
REFERENCE
REV. DATE: JUL 01/21
SECTION:
2 -29
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
292400-03-1
ZONE
210 AUXILIARY HYDRAULIC POWER
AF
FNC
630
OPERATIONAL CHECK OF MANUAL RAT DEPLOYMENT FOLLOWED
BY FUNCTIONAL CHECK OF RAT OPERATION AND INSPECTION
OF FILTER ELEMENT BY REFERENCE TO DIFFERENTIAL
PRESSURE INDICATOR.
ACCESS: 196BB
292400-04-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
197CB
633HB
I:
24 MO
OR
12000 FH
SOURCE
CMR**
MRB 8
AF
RST
REMOVE RAT (INCLUDING ACTUATOR, MANIFOLD, HYDRAULIC
PUMP AND TURBINE-LOWER GEARBOX ASSEMBLY), FOR
OVERHAUL AND REPLACE WITH SERVICEABLE UNITS.
292400-720-801
MRB REFERENCE:
29.20.00/06
T:
20 YE
I:
20 YE
SEMR
292452-960-801
190 HYDRAULIC SYSTEM DATA ACQUISITION / INTERFACEAF
210 AND INDICATING
OPC
I:
4000 FH
MRB 9
293100-200-801
MRB REFERENCE:
29.30.00/01
CROSS CHECK FLUID LEVEL ON EACH RESERVOIR, ON ECAM
HYDRAULIC PAGE AND GROUND SERVICE PANEL INDICATOR.
ACCESS: 197CB
293000-02-1
147 HYDRAULIC SYSTEM DATA ACQUISITION / INTERFACEAF
190 AND INDICATING
210
OPERATIONAL CHECK OF RESERVOIRS LOW AIR PRESSURE
WARNING.
ACCESS: 195BB
293000-03-1
196BB
197CB
734
OPC
I:
24 MO
MRB 9
MRB REFERENCE:
29.30.00/03
OPC
I:
24 MO
MRB 9
E N D
SYSTEMS, APU AND POWER PLANT : HYDRAULIC POWER
2
2
0.75 ALL
0.75
*
0.22
2
4.00 ALL
*
2.50
1
1
0.05 ALL
0.05
*
0.01
1
1
1
0.20 ALL
0.20
0.20
*
0.33
1
0.10 ALL
APPLICABILITY
293100-740-802
MRB REFERENCE:
29.30.00/02
OPERATIONAL CHECK OF OVERHEAT DETECTION SYSTEM.
* * * * *
293100-710-802
744
210 HYDRAULIC SYSTEM DATA ACQUISITION / INTERFACEAF
AND INDICATING
M/H
SEMR REFERENCE:
292400-00001-1-E
PREP.: FIXED FLAP TRACK FAIRING Z633;
293000-01-1
MEN
CMR REFERENCE:
292000-00001-1-C
633JR
633 RAM AIR TURBINE
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -29
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
301100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
500 WING ICE PROTECTION
EL
DET
600
DETAILED INSPECTION OF TELESCOPIC DUCTS, FLEXIBLE
SLAT INTERCONNECTION SLEEVES AND, IN WING LEADING
EDGE, ANTI-ICING DUCT COUPLINGS, CLAMPS AND
ATTACHMENT POINTS.
I:
48 MO
SOURCE
MRB 9
REFERENCE
301100-200-801
MEN
M/H
1
1
0.50 ALL
0.50
*
*
3.30
3.30
1
1
0.15 GE
0.15
*
*
0.15
0.15
1
1
0.30 GE
0.30
*
*
1.05
1.05
1
0.10 GE
APPLICABILITY
MRB REFERENCE:
30.11.00/01
NOTE:
ETOPS RELEVANT
ACCESS: 522JB
622JB
302100-02-1
522LB
622LB
522NB
622NB
522RB
622RB
523CB
623CB
523EB
623EB
410 ENGINE AIR INTAKE ICE PROTECTION
EN
DET
420
DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY
DUCTS AND ASSOCIATED HARDWARE IN CORE AND FAN
COMPARTMENTS.
I:
18 MO
MRB 6
302100-200-802
MRB REFERENCE:
30.21.01/01
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
302100-05-1
416AR
426AR
417AL
427AL
411 ENGINE AIR INTAKE ICE PROTECTION
EN
421
VISUAL CHECK OF INLET COWL ANTI-ICE SUPPLY DUCT
(BETWEEN SWIRL NOZZLE AND AFT BULKHEAD).
VCK
I:
72 MO
MRB 8
302100-200-806
MRB REFERENCE:
30.21.01/03
NOTE:
ETOPS RELEVANT
ACCESS: 411AL
421AL
302100-06-1
411AR
421AR
411BL
421BL
210 ENGINE AIR INTAKE ICE PROTECTION
EN
OPC
I:
48 MO
MRB 8
OPERATIONAL CHECK OF THE ENGINE AIR INTAKE ICE
PROTECTION.
302100-710-814
MRB REFERENCE:
30.21.01/04
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ICE & RAIN PROTECTION
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-30
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
302100-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
ETOPS RELEVANT
302102-01-1
210 ENGINE AIR INTAKE ICE PROTECTION
EN
OPC
I:
48 MO
MRB 8
OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE
PROTECTION.
302100-710-815
1
0.17 PW
1
1
0.20 PW
0.20
*
*
0.80
0.80
1
0.33 TRENT 700
1
1
0.42 TRENT 700
0.42
*
*
0.60
0.60
MRB REFERENCE:
30.21.02/01
NOTE:
ETOPS RELEVANT
302102-02-1
411 ENGINE AIR INTAKE ICE PROTECTION
EN
VCK
421
VISUAL CHECK OF NAI DUCT IN INLET COMPARTMENT AND FAN
ZONE.
I:
72 MO
MRB 8
302100-210-802
MRB REFERENCE:
30.21.02/02
NOTE:
ETOPS RELEVANT
ACCESS: 411AL
421AL
302103-01-1
411AR
421AR
210 ENGINE AIR INTAKE ICE PROTECTION
EN
OPC
I:
48 MO
MRB 8
OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE
PROTECTION.
302100-710-816
MRB REFERENCE:
30.21.03/01
NOTE:
ETOPS RELEVANT
302103-02-1
411 ENGINE AIR INTAKE ICE PROTECTION
421
VISUAL CHECK OF INTERBULKHEAD.
EN
VCK
I:
72 MO
MRB 8
302100-210-803
MRB REFERENCE:
30.21.03/02
NOTE:
ETOPS RELEVANT
ACCESS: 411AL
421AL
SYSTEMS, APU AND POWER PLANT : ICE & RAIN PROTECTION
REV. DATE: JUL 01/21
SECTION:
2-30
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
302106-N1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 ENGINE AIR INTAKE ICE PROTECTION
EN
OPC
I:
96 MO
SOURCE
MRB 8
OPERATIONAL CHECK OF NAI SYSTEM.
120 PROBE ICE PROTECTION
EL
FNC
I:
24 MO
MRB 9
FUNCTIONAL CHECK OF HEATER INSULATION RESISTANCE OF
THE PITOT PROBES.
304600-01-1
120 ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTIONAF
OPC
130
150 OPERATIONAL CHECK OF ESCAPE SLIDE LOCKING MECHANISM
170 ICE PROTECTION.
ACCESS: 132AZ
152PW
162ZW
* * * * *
302100-710-811
303100-720-802
M/H
APPLICABILITY
1
0.02 TRENT 7000
1
0.30 ALL
1
1
1
1
0.05
0.05
0.05
0.05
MRB REFERENCE:
30.31.00/01
I: 12000 FH
MRB 9
304600-710-801
MRB REFERENCE:
30.46.00/01
132MW
E N D
MEN
MRB REFERENCE:
30.21.06/01-RN
NOTE:
ETOPS RELEVANT
303100-01-1
REFERENCE
*
*
*
A330-200
POST 40335
PRE 51642
PRE 51617
OR
0.11 A330-300
0.10 POST 40335
0.02 PRE 51642
PRE 51617
* * * * *
SYSTEMS, APU AND POWER PLANT : ICE & RAIN PROTECTION
REV. DATE: JUL 01/21
SECTION:
2-30
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
312100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 ELECTRICAL CLOCK
EL
DIS
I:
24 MO
SOURCE
MRB 9
DISCARD CLOCK BATTERY.
313300-01-1
312121-920-802
MRB REFERENCE:
31.21.00/01
PREP.: CLOCK;
R
REFERENCE
312 DIGITAL FLIGHT DATA RECORDING SYSTEM
AV
DIS
I:
CE
NOTE
MRB 9
REMOVE ULB FOR IN SHOP ULB BATTERY DISCARD.
313355-920-801
ACCESS: 312AR
313300-02-1
210 DIGITAL FLIGHT DATA RECORDING SYSTEM
AV
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU.
R
313300-03-1
312 DIGITAL FLIGHT DATA RECORDING SYSTEM
AV
OPC
I:
36 MO
MRB 9
ACCESS: 312AR
AV
OPC
I:
24 MO
MRB
DOWNLOAD AND READ OUT OF DFDR DATA TO ENSURE RECORDED
PARAMETERS MEET THE RANGE AND ACCURACIES REQUIRED BY
14 CFR PART 121, APPENDIX M.
R
313300-05-1
120 DIGITAL FLIGHT DATA RECORDING SYSTEM
210
OPERATIONAL CHECK OF WGL-QAR INTERLOCK AND
TRANSMISSION LOGIC.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : INSTRUMENTS
313300-710-803
313300-720-802
MRB REFERENCE:
31.33.00/03
310 DIGITAL FLIGHT DATA RECORDING SYSTEM
EL
APPLICABILITY
1
0.10 IF CLOCK FITTED
WITH BATTERY
*
0.40
1
0.20 PRE
*
0.01
1
0.15 PRE
208191
1
0.25 PRE
208191
*
0.01
1
0.50 FAA
1
1
0.20 POST 56807
0.20 (31-3130)
PRE 206186
(31-3234)
PRE 208191
208191
MRB REFERENCE:
31.33.00/02
OPERATIONAL CHECK OF ULB.
313300-04-1
M/H
MRB REFERENCE:
31.33.00/01
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
R
MEN
OPC
313300-710-815
MRB REFERENCE:
MRB SEC_F
I: 24000 FH
MRB 8
313300-710-820
MRB REFERENCE:
31.33.00/05
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-31
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
313300-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
POST 58513
(31-3181),
(31-3185)
PRE 206186
(31-3234)
PRE 208191
R
N
313300-06-1
313400-01-1
120 DIGITAL FLIGHT DATA RECORDING SYSTEM
210
OPERATIONAL CHECK OF WGL-DAR INTERLOCK AND
TRANSMISSION LOGIC.
EL
OPC
I: 24000 FH
MRB 8
210 RECORDING AND AIRCRAFT LOCATING SYSTEM
AV
OPC
I:
36 MO
MRB 8
AV
DIS
I:
60 MO
NOTE
OPC
I:
24 MO
313600-710-826
1
1
0.20 POST 55048
0.20 (31-3109),
(31-3167)
PRE 208191
OR
POST 56293
(31-3119),
(31-3142),
(31-3184),
(31-3193),
(31-3215),
(31-3233)
PRE 208191
MRB REFERENCE:
31.34.00/01
1
TBD POST 208191
MRB 8
MRB REFERENCE:
31.34.00/02
1
TBD POST 208191
MRB 9
MRB REFERENCE:
31.34.00/03
1
1
TBD POST 208191
TBD
MRB REFERENCE:
31.33.00/04
OPERATIONAL CHECK OF ADFR ELT FUNCTIONALITY.
N
313400-02-1
325 RECORDING AND AIRCRAFT LOCATING SYSTEM
REMOVE ADFR FOR IN SHOP ADFR ELT BATTERY DISCARD.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
N
313400-03-1
121 RECORDING AND AIRCRAFT LOCATING SYSTEM
122
OPERATIONAL CHECK OF CVDR ULB.
SYSTEMS, APU AND POWER PLANT : INSTRUMENTS
AV
REV. DATE: JUL 01/21
SECTION:
2-31
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
313400-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
121 RECORDING AND AIRCRAFT LOCATING SYSTEM
122
DISCARD OF CVDR ULB BATTERY.
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
AV
DIS
I:
60 MO
NOTE
MRB 9
MRB REFERENCE:
31.34.00/04
1
1
TBD POST 208191
TBD
AV
OPC
I: 24000 FH
MRB 9
MRB REFERENCE:
31.34.00/05
1
TBD POST 208191
AV
RST
I:
60 MO
NOTE
MRB 6,8
MRB REFERENCE:
31.34.00/06
1
TBD POST 208191
DIS
I:
120 MO
NOTE
MRB 8
MRB REFERENCE:
31.34.00/07
1
TBD POST 208191
OPC
I: 34000 FH
MRB 8
315000-740-803
1
0.10 ALL
1
0.10 ALL
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
N
313400-05-1
210 RECORDING AND AIRCRAFT LOCATING SYSTEM
OPERATIONAL CHECK OF RECORDING RELAY LOGIC.
N
313400-06-1
325 RECORDING AND AIRCRAFT LOCATING SYSTEM
REMOVE RRU FOR IN SHOP FUNCTIONAL CHECK OF RECORDER
RELEASE UNIT MECHANISM AND FUNCTIONAL CHECK OF
HYDROSTATIC SWITCHES.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
N
313400-07-1
325 RECORDING AND AIRCRAFT LOCATING SYSTEM
AV
REMOVE RRU FOR IN SHOP GAS CARTRIDGE DISCARD.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
315000-01-1
210 CENTRAL WARNING SYSTEM
AV
OPERATIONAL CHECK OF SLAT AND FLAP SENSOR CIRCUIT VIA
MCDU.
315000-02-1
210 CENTRAL WARNING SYSTEM
AV
OPC
MRB REFERENCE:
31.50.00/03
I: 34000 FH
MRB 8
OPERATIONAL CHECK OF DMC OUTPUT CIRCUITS TO FWC'S.
SYSTEMS, APU AND POWER PLANT : INSTRUMENTS
315000-740-804
MRB REFERENCE:
31.50.00/04
REV. DATE: JUL 01/21
SECTION:
2 -31
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
316000-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 ELECTRONIC INSTRUMENT SYSTEM
AV
OPC
I:
24 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF PFD/ND AND ECAM/ND MANUAL
TRANSFER.
316000-02-1
210 ELECTRONIC INSTRUMENT SYSTEM
AV
210 ELECTRONIC INSTRUMENT SYSTEM
AV
OPC
I:
24 MO
MRB 9
210 ELECTRONIC INSTRUMENT SYSTEM
AV
OPC
I:
48 MO
MRB 9
OPC
210 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD
TECHNOLOGY)
AV
OPC
I: 34000 FH
MRB 8
1
0.25 PRE 50161
(31-3056),
(31-3253)
PRE 51153
(31-3056),
(31-3057),
(31-3253)
1
0.20 PRE 50161
(31-3056),
(31-3253)
PRE 51153
(31-3056),
(31-3057),
(31-3253)
316000-720-801
1
0.20 PRE 50161
(31-3056),
(31-3253)
PRE 51153
(31-3056),
(31-3057),
(31-3253)
1
0.15 POST 50161
(31-3056),
(31-3253)
OR
POST 51153
(31-3056),
(31-3057),
(31-3253)
MRB REFERENCE:
31.60.00/05
I:
24 MO
MRB 9
316000-710-809
MRB REFERENCE:
31.60.01/01
OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL
TRANSFER.
SYSTEMS, APU AND POWER PLANT : INSTRUMENTS
316000-710-806
REV. DATE: JUL 01/21
SECTION:
2 -31
APPLICABILITY
0.20 PRE 50161
(31-3056),
(31-3253)
PRE 51153
(31-3056),
(31-3057),
(31-3253)
MRB REFERENCE:
31.60.00/03
OPERATIONAL CHECK OF EFIS OFFSIDE AND ECAM NON ACTIVE
MONITORING CIRCUITS.
316001-01-1
316000-710-805
M/H
1
MRB REFERENCE:
31.60.00/02
OPERATIONAL CHECK OF CORRECT EFIS AND ECAM TRANSFER
WHEN BUSBAR 105XP IS LOST.
316000-04-2
316000-710-804
MEN
MRB REFERENCE:
31.60.00/01
OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER.
316000-03-1
REFERENCE
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
316001-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
121 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD
210 TECHNOLOGY)
AV
OPC
I:
72 MO
SOURCE
MRB 9
210 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD
TECHNOLOGY)
AV
OPC
I:
24 MO
MRB 8
E N D
SYSTEMS, APU AND POWER PLANT : INSTRUMENTS
316000-710-810
MRB REFERENCE:
31.60.01/04
OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER.
* * * * *
316000-710-807
MEN
M/H
APPLICABILITY
1
1
0.10 POST 50161
0.10 (31-3056),
(31-3253)
OR
POST 51153
(31-3056),
(31-3057),
(31-3253)
1
0.25 POST 50161
(31-3056),
(31-3253)
OR
POST 51153
(31-3056),
(31-3057),
(31-3253)
MRB REFERENCE:
31.60.01/03
OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN
BUSBAR 105XP IS LOST.
316001-04-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-31
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
321000-03-1
321000-04-1
321000-05-1
R
321100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
731 MAIN GEAR AND DOORS
741
LUBRICATION OF MLG AND DOORS.
AF
731 MAIN GEAR AND DOORS
741
LUBRICATION OF MLG BOGIE BEAM PIVOT PIN.
AF
LUB
LUB
I:
I:
731 MAIN GEAR AND DOORS
AF
LUB
741
LUBRICATION OF MLG SHORTENING MECHANISM SM8 AND SM9
HINGE JOINTS.
I:
731 MAIN GEAR
NDT SDI
741
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG (OFF
AIRCRAFT).
I:
4 MO
OR
500 FC
SOURCE
MRB 5,8
MRB 6
4 MO
OR
250 FC
MRB 6
321100-01-2
731 MAIN GEAR
NDT SDI
741
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG (OFF
AIRCRAFT).
I:
12 YE
OR
20000 FC
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
122232-600-820
MRB REFERENCE:
32.11.00/02
MRB 5,8
MRB CPCP
321111-920-801
APPENDIX APX 7
MRB REFERENCE:
32.11.00/06
321108-02-1
321114-02-1
321121-01-1
321130-01-1
321132-01-1
MRB 5,8
MRB CPCP
PREP.: AIRCRAFT JACKING;
MAIN LANDING GEAR Z731;
MAIN LANDING GEAR Z741;
* * * * *
122232-640-801
MRB REFERENCE:
32.11.00/15
PREP.: AIRCRAFT JACKING;
MAIN LANDING GEAR Z731;
MAIN LANDING GEAR Z741;
N
122232-600-817
MEN
M/H
APPLICABILITY
1
1
1.20 ALL
1.20
1
1
0.15 ALL
0.15
1
1
0.20 PRE 54500
0.20 PRE 58091
(32-3227)
OR
PRE 54500
PRE 58099
(32-3227)
0
0
N/A A330-200
N/A OR
A330-200F
OR
A330-300
42.50 OR
A330-800
PRE 208040
OR
A330-900
PRE 208040
MRB REFERENCE:
32.11.00/01
32.30.00/01
32.30.00/03
32.40.00/12
4 MO
OR
50 FC
10 YE
OR
20000 FC
REFERENCE
*
321111-920-801
APPENDIX APX 7
1
1
MRB REFERENCE:
32.11.00/21
321190-01-1
321191-01-1
321192-01-1
*
TBD A330-800
TBD POST 208040
OR
A330-900
POST 208040
42.50
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
321100-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
321194-01-1
R
321100-02-1
321100-03-1
321100-04-1
321100-05-1
321100-14-1
R
321100-24-1
731 MAIN GEAR
AF
741
FUNCTIONAL CHECK OF MLG BOGIE BEAM PITCH TRIMMER
CONTROL MANIFOLD HYDRAULIC FUSE (OFF AIRCRAFT).
FNC
731 MAIN GEAR
AF
741
FUNCTIONAL CHECK OF MLG SHOCK ABSORBER NITROGEN
CHARGE PRESSURE.
FNC
731 MAIN GEAR
741
SERVICE MLG SHOCK ABSORBER.
SVC
AF
I:
12 YE
MRB 9
321100-720-802
MRB REFERENCE:
32.11.00/07
I:
24 MO
MRB 6
321100-220-819
1
1
0.75 ALL
0.75
1
1
0.50 ALL
0.50
2
2
1.66 ALL
1.66
1
1
0.20 ALL
0.20
1
1
0.05 ALL
0.05
MRB REFERENCE:
32.11.00/03
I:
42 MO
MRB 6
321100-220-803
MRB REFERENCE:
32.11.00/04
731 MAIN GEAR
AF
FNC
741
FUNCTIONAL CHECK OF MLG TORQUE LINKS FOR EXCESSIVE
PLAY.
I:
731 MAIN GEAR
AF
741
GENERAL VISUAL INSPECTION OF BOGIE PITCH TRIMMER
CONTROL MANIFOLD.
I:
GVI
731 MAIN GEAR
AF
SDI
741
SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN
MLG AIRFRAME ATTACHMENT FITTINGS.
72 MO
MRB 6
321127-200-801
MRB REFERENCE:
32.11.00/05
2000 FH
MRB 6
321100-210-831
MRB REFERENCE:
32.11.00/11
I:
10 YE
OR
20000 FC
MRB 5,8
321100-280-801
MRB REFERENCE:
32.11.00/12
1
1
NOTE:
- TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED
MLG REMOVAL.
PREP.: MAIN LANDING GEAR REMOVED;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
*
1.00 A330-200
1.00 OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208040
OR
20.00 A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
321100-24-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PRE
N
321100-24-2
571 MAIN GEAR
NDT SDI
671
SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN
MLG AIRFRAME ATTACHMENT FITTINGS.
I:
12 YE
OR
20000 FC
MRB 5,8
321100-280-801
MRB REFERENCE:
32.11.00/23
1
1
208040
TBD A330-800
TBD POST 208040
OR
A330-900
POST 208040
NOTE:
- TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED
MLG REMOVAL.
PREP.: MAIN LANDING GEAR REMOVED;
321100-25-1
R
321100-30-1
*
731 MAIN GEAR
AF
741
LUBRICATION OF MLG SHOCK ABSORBER LOWER BEARING.
LUB
731 MAIN GEAR
NDT
741
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG
RETRACTION ACTUATOR (OFF AIRCRAFT).
SDI
I:
I:
4 MO
OR
500 FC
10 YE
OR
17000 FC
MRB 6
321100-30-2
731 MAIN GEAR
NDT
741
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG
RETRACTION ACTUATOR (OFF AIRCRAFT).
MRB 5,8
MRB CPCP
I:
12 YE
OR
20000 FC
MRB 5,8
MRB CPCP
321100-280-810
APPENDIX APX 7
MRB REFERENCE:
32.11.00/24
32.30.00/18
321195-01-1
PREP.: MLG RETRACTION ACTUATOR REMOVED;
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
321100-280-810
APPENDIX APX 7
MRB REFERENCE:
32.11.00/17
32.30.00/18
321140-01-1
SDI
1
1
0.10 PRE 45414
0.10 (32-3072)
0
0
N/A A330-200
N/A OR
A330-200F
OR
A330-300
5.00 OR
A330-800
PRE 208040
OR
A330-900
PRE 208040
MRB REFERENCE:
32.11.00/13
PREP.: RETRACTION ACTUATOR REMOVED;
N
122232-640-803
20.00
REV. DATE: JUL 01/21
SECTION:
2 -32
*
1
1
*
TBD A330-800
TBD POST 208040
OR
A330-900
POST 208040
TBD
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
R
321100-31-1
321100-32-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
731 MAIN GEAR
NDT
741
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG
RETRACTION LINK BUSHES, BEARINGS AND PINS (OFF
AIRCRAFT).
SDI
I:
10 YE
OR
15000 FC
SOURCE
MRB 5
REFERENCE
321100-280-812
APPENDIX APX 7
541 MAIN GEAR
NDT SDI
641
731 SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG AFT
741 PINTLE PIN & NUT (OFF AIRCRAFT).
I:
10 YE
OR
20000 FC
MRB 5,8
MRB CPCP
321100-280-813
APPENDIX APX 7
MRB REFERENCE:
32.11.00/19
321125-02-1
PREP.: MLG DOORS OPEN;
321100-32-2
541 MAIN GEAR
NDT SDI
641
731 SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG AFT
741 PINTLE PIN & NUT (OFF AIRCRAFT).
I:
12 YE
OR
20000 FC
MRB
MRB 5,8
321100-280-813
APPENDIX APX 7
MRB REFERENCE:
32.11.00/25
321193-01-1
PREP.: MLG DOORS OPEN;
321100-33-1
541 MAIN GEAR
NDT
641
731 SPECIAL DETAILED INSPECTION OF MLG SHORTENING
741 MECHANISM (SM) 1 PIN.
SDI
I:
10 YE
OR
20000 FC
MRB 6
321100-280-814
MRB REFERENCE:
32.11.00/20
PREP.: MLG DOORS OPEN;
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
1
1
1
1
*
NOTE:
TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED MLG
REMOVAL.
R
0
0
MRB REFERENCE:
32.11.00/18
NOTE:
TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED MLG
REMOVAL.
N
MEN
M/H
N/A A330-200
N/A OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208040
OR
A330-900
PRE 208040
0.42
0.42
0.42
0.42
A330-200
OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208040
OR
TBD A330-900
PRE 208040
1
1
1
1
0.42
0.42
0.42
0.42
*
TBD
1
1
1
1
0.85
0.85
0.85
0.85
*
APPLICABILITY
A330-800
POST 208040
OR
A330-900
POST 208040
A330-200
OR
A330-200F
OR
A330-300
TBD OR
A330-800
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
321100-33-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PRE 208040
OR
A330-900
PRE 208040
N
321100-33-2
541 MAIN GEAR
NDT
641
731 SPECIAL DETAILED INSPECTION OF MLG SHORTENING
741 MECHANISM (SM) 1 PIN.
SDI
I:
12 YE
OR
20000 FC
MRB 6
321100-280-814
MRB REFERENCE:
32.11.00/22
PREP.: MLG DOORS OPEN;
322000-01-1
711 NOSE GEAR AND DOORS
AF
LUB
I:
LUBRICATION OF NLG AND DOORS.
R
322100-02-1
711 NOSE GEAR
NDT
SDI
I:
SPECIAL DETAILED INSPECTION (OVERHAUL) OF NLG (OFF
AIRCRAFT).
4 MO
OR
500 FC
10 YE
OR
20000 FC
MRB 5,8
322100-02-2
711 NOSE GEAR
NDT
SDI
MRB 5,8
MRB CPCP
SPECIAL DETAILED INSPECTION (OVERHAUL) OF NLG (OFF
AIRCRAFT).
12 YE
OR
20000 FC
MRB 5,8
MRB CPCP
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
322111-920-801
APPENDIX APX 7
MRB REFERENCE:
32.21.00/11
32.50.00/06
322190-01-1
PREP.: AIRCRAFT JACKING;
NOSE LANDING GEAR;
* * * * *
322111-920-801
APPENDIX APX 7
MRB REFERENCE:
32.21.00/05
32.50.00/03
322107-02-1
322108-01-1
322112-01-1
I:
TBD
TBD
TBD
TBD
*
TBD
1
A330-800
POST 208040
OR
A330-900
POST 208040
0.60 ALL
MRB REFERENCE:
32.21.00/01
32.30.00/01
32.30.00/03
32.50.00/01
PREP.: AIRCRAFT JACKING;
NOSE LANDING GEAR;
N
122232-600-819
1
1
1
1
0
*
1
*
N/A A330-200
OR
A330-200F
OR
A330-300
17.50 OR
A330-800
PRE 208041
OR
A330-900
PRE 208041
TBD A330-800
POST 208041
OR
A330-900
POST 208041
17.50
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
322100-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
322191-01-1
322192-01-1
322100-03-1
711 NOSE GEAR SHOCK ABSORBER
AF
SVC
I:
42 MO
MRB 6
SERVICE NLG SHOCK ABSORBER.
322100-04-1
711 NOSE GEAR
AF
FNC
I:
24 MO
MRB 6
711 NOSE GEAR TORQUE LINKS
AF
FNC
322100-720-801
I:
48 MO
MRB 6
322127-200-801
1
0.50 ALL
1
0.60 ALL
*
2.50
MRB REFERENCE:
32.21.00/03
PREP.: AIRCRAFT JACKING (NLG ONLY);
322100-11-1
1.16 ALL
MRB REFERENCE:
32.21.00/02
FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE
PLAY.
R
2
MRB REFERENCE:
32.21.00/04
FUNCTIONAL CHECK NLG SHOCK ABSORBER NITROGEN CHARGE
PRESSURE.
322100-05-1
322100-220-802
711 NOSE GEAR
AF
SDI
I:
SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN
NLG AIRFRAME ATTACHMENT FITTINGS.
10 YE
OR
20000 FC
MRB 5,8
322100-280-801
1
MRB REFERENCE:
32.21.00/08
NOTE:
- TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED
NLG REMOVAL.
PREP.: NOSE LANDING GEAR REMOVED;
N
322100-11-2
*
711 NOSE GEAR
NDT
SDI
SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN
NLG AIRFRAME ATTACHMENT FITTINGS.
I:
12 YE
OR
20000 FC
MRB 5,8
322100-280-801
MRB REFERENCE:
32.21.00/12
1
1.10 A330-200
OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208041
OR
15.00 A330-900
PRE 208041
TBD A330-800
POST 208041
OR
A330-900
POST 208041
NOTE:
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-32
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
322100-11-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
- TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED
NLG REMOVAL.
PREP.: NLG REMOVED;
R
322100-12-1
711 NOSE GEAR
*
NDT
SDI
I:
SPECIAL DETAILED INSPECTION (OVERHAUL) OF NLG
RETRACTION ACTUATOR (OFF AIRCRAFT).
10 YE
OR
20000 FC
MRB 5,8
MRB CPCP
MRB REFERENCE:
32.21.00/10
32.30.00/17
322114-01-1
PREP.: RETRACTION ACTUATOR REMOVED;
N
322100-12-2
711 NOSE GEAR
NDT
SDI
I:
SPECIAL DETAILED INSPECTION (OVERHAUL) OF NLG
RETRACTION ACTUATOR (OFF AIRCRAFT).
12 YE
OR
20000 FC
MRB 5,8
MRB CPCP
323000-21-1
123 NORMAL EXTENSION AND RETRACTION POSITION AND AF
DET
147 WARNING
148
700 DETAILED INSPECTION OF LANDING GEAR UPLOCK UNITS,
DOOR UPLOCK UNITS AND ROLLERS.
I:
123 NORMAL EXTENSION AND RETRACTION POSITION AND AF
147 WARNING
148
DETAILED INSPECTION OF LANDING GEAR DOOR HINGE
BEARINGS, ATTACHMENT LUG BUSHES AND PINS.
I:
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
DET
322100-280-802
APPENDIX APX 7
MRB REFERENCE:
32.21.00/13
32.30.00/17
322193-01-1
PREP.: NLG RETRACTION ACTUATOR REMOVED;
323000-20-1
322100-280-802
APPENDIX APX 7
24 MO
OR
3000 FC
MRB 5,8
12 YE
MRB 5,8
323100-220-801
MRB REFERENCE:
32.30.00/14
323100-220-802
MRB REFERENCE:
32.30.00/15
REV. DATE: JUL 01/21
SECTION:
2 -32
0
*
1
*
TBD
N/A A330-200
OR
A330-200F
OR
A330-300
5.00 OR
A330-800
PRE 208041
OR
A330-900
PRE 208041
TBD A330-800
POST 208041
OR
A330-900
POST 208041
TBD
1
1
1
1
0.30 ALL
0.30
0.30
0.30
1
1
1
0.50 ALL
0.50
0.50
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
323000-22-1
323100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
123 NORMAL EXTENSION AND RETRACTION POSITION AND AF
DET
147 WARNING
148
DETAILED INSPECTION OF LANDING GEAR DOOR ACTUATING
CYLINDER BEARINGS, ATTACHMENT LUG BUSHES AND PINS.
I:
700 NORMAL EXTENSION AND RETRACTION
I:
AF
VCK
12 YE
SOURCE
MRB 5,8
210 NORMAL EXTENSION AND RETRACTION
AF
5000 FH
MRB 9
210 NORMAL EXTENSION AND RETRACTION
AF
323100-210-801
OPC
I:
72 MO
MRB 9
323100-710-803
FNC
I:
72 MO
MRB 9
323100-720-802
AF
1
1
1
0.50 ALL
0.50
0.50
1
0.60 ALL
1
0.05 ALL
2
1.16 ALL
*
0.60
2
1.20 ALL
1
0.76 ALL
*
2.50
APPLICABILITY
MRB REFERENCE:
32.30.00/11
PREP.: APU RUNNING;
700 FREE FALL EXTENSION
M/H
MRB REFERENCE:
32.30.00/09
FUNCTIONAL CHECK OF LANDING GEAR ISOLATION SAFETY
VALVE.
323300-03-1
MEN
MRB REFERENCE:
32.30.00/04
OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK.
323100-03-1
323100-220-803
MRB REFERENCE:
32.30.00/16
VISUAL CHECK OF DOWN LOCK SPRINGS ON ALL LANDING
GEARS.
323100-02-1
REFERENCE
OPC
I:
3400 FH
CMR*
MRB 8
OPERATIONAL CHECK OF LANDING GEAR FREE-FALL SYSTEM.
323300-710-809
CMR REFERENCE:
323000-00001-1-C
MRB REFERENCE:
32.30.00/08
323300-04-1
700 FREE FALL EXTENSION
AF
FNC
I:
6 YE
MRB 8
FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION.
MRB REFERENCE:
32.11.00/14
32.21.00/09
32.30.00/12
PREP.: AIRCRAFT JACKING;
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
323300-720-804
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
324000-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
195 BRAKE ACCUMULATORS
AF
FNC
I:
1000 FH
SOURCE
MRB 9
FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON
ALTERNATE PARKING BRAKE ACCUMULATORS.
REFERENCE
324000-210-805
324000-04-1
731 BRAKE ACCUMULATORS
AF
FNC
741
FUNCTIONAL CHECK OF NORMAL AND ALTERNATE BRAKE RETURN
ACCUMULATORS NITROGEN PRESSURES BY READING GAUGES.
I:
210 BRAKES AND WHEELS
I:
AF
M/H
APPLICABILITY
1
0.10 ALL
*
0.01
1
1
0.05 ALL
0.05
2
1.00 POST 46231
(32-3083)
MRB REFERENCE:
32.40.00/06
ACCESS: 195BB
324000-03-1
MEN
OPC
2000 FH
MRB 6,9
324000-210-804
MRB REFERENCE:
32.40.00/04
4000 FH
CMP
MRB 9
OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE.
324400-710-802
CMP REFERENCE:
32-2-0000-001
MRB REFERENCE:
32.40.00/10
N
324000-05-1
324000-19-1
210 BRAKES AND WHEELS
AF
OPC
700
OPERATIONAL CHECK OF THE RETRACTION BRAKING SYSTEM.
I: 61000 FH
731 BRAKES AND WHEELS
741
DETAILED INSPECTION OF MLG AXLE SLEEVES.
I:
AF
DET
CMR*
700 BRAKES AND WHEELS
24 MO
MRB 9
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
324000-220-803
MRB REFERENCE:
32.40.00/14
AF
GVI
1
1
CMR REFERENCE:
324000-00001-1-C
PREP.: AIRCRAFT JACKING;
MLG BRAKES;
MLG SLEEVES;
MLG WHEELS;
324100-03-1
324000-710-806
I:
3 DY
MRB 6,9
324100-210-803
1
1
*
1
TBD A330-900
TBD POST 207873
OR
A330-900
POST 208006
OR
A330-900
POST 208007
0.80 ALL
0.80
28.50
0.30 ALL
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
324100-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
324300-01-1
700 TYRES
AF
FNC
I:
3 DY
MRB 9
I:
122 ALTERNATE BRAKE HYDRAULIC RESERVOIR
I:
AF
FNC
42 FC
MRB 9
24 MO
MRB 6
AF
VCK
I:
210 PARKING BRAKING
AF
OPC
210 TYRE PRESSURE SYSTEM
AF
FNC
700
FUNCTIONAL CHECK OF TPIS AND CROSS CHECK WITH TYRE
PRESSURE GAUGE READING.
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
0.20 ALL
1
1
0.05 ALL
0.05
324300-210-802
1
0.20 ALL
*
0.06
8000 FH
MRB 9
324314-200-801
1
0.20 POST 47210
(32-3086)
1
0.20 ALL
1
1
0.15 IF TPIS INSTALLED
0.15
MRB REFERENCE:
32.40.00/11
I:
OPERATIONAL CHECK OF PARKING BRAKE CONTROL VALVE
MOTORS 1 AND 2.
324900-02-1
324000-210-802
811
147 ALTERNATE BRAKE DUAL VALVE
1
MRB REFERENCE:
32.40.00/05
VISUAL CHECK OF BRAKE DUAL DISTRIBUTION VALVE (BDDV)
DRAIN TUBE FOR THE ACCUMULATION OF WATER.
324500-01-1
324100-220-802
MRB REFERENCE:
32.40.00/01
FUNCTIONAL CHECK OF BRAKE LOW PRESSURE RESERVOIR
FLUID LEVEL.
324314-01-1
APPLICABILITY
MRB REFERENCE:
32.40.00/02
730 BRAKE UNITS
AF
VCK
740
VISUAL CHECK OF THE BRAKE HEAT PACK FOR WEAR BY USE
OF THE WEAR INDICATOR (PARKING BRAKE APPLIED).
ACCESS: 132AZ
M/H
MRB REFERENCE:
32.40.00/07
32.40.00/08
32.40.00/09
FUNCTIONAL CHECK OF TYRE PRESSURES.
324200-01-1
MEN
* * * * *
GENERAL VISUAL INSPECTION OF TYRES, WHEELS AND
BRAKES.
324100-04-1
REFERENCE
I:
24 MO
OR
3000 FC
MRB 9
1000 FH
MRB 9
324500-710-803
MRB REFERENCE:
32.40.00/13
324900-220-802
MRB REFERENCE:
32.40.00/03
REV. DATE: JUL 01/21
SECTION:
2-32
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
325000-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
710 STEERING
AF
OPC
I:
42 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF ALTERNATE NOSE WHEEL STEERING
SYSTEM.
325100-02-1
710 NOSE WHEEL STEERING
AF
FNC
325300-01-1
210 STEERING ANGLE PROTECTION
AF
FNC
I:
24 MO
MRB 9
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
325100-720-810
M/H
APPLICABILITY
1
0.20 A330-200
POST 200917
OR
A330-300
POST 200917
2
0.23 ALL
2
0.40 A330-200
POST 43442
(32-3030)
PRE 56814
(32-3234)
PRE 58794
OR
A330-200
POST 201082
(32-3246)
OR
A330-200F
PRE 56814
(32-3234)
PRE 58794
OR
A330-200F
POST 201082
(32-3246)
OR
A330-300
POST 43442
(32-3030)
PRE 56814
(32-3234)
PRE 58794
OR
A330-300
POST 201082
(32-3246)
OR
A330-800
MRB REFERENCE:
32.50.00/02
I:
24 MO
MRB 9
FUNCTIONAL CHECK OF OVERSTEER INDICATION SYSTEM.
* * * * *
325100-710-804
MEN
MRB REFERENCE:
32.50.00/05
FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON NOSE
WHEEL STEERING ACCUMULATOR.
R
REFERENCE
325300-720-801
MRB REFERENCE:
32.53.00/02
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -32
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
325300-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 201082
(32-3246)
OR
A330-900
POST 201082
(32-3246)
325300-02-1
210 STEERING ANGLE PROTECTION
EL
OPC
710
OPERATIONAL CHECK OF COCKPIT AND NLG WARNING LAMPS.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
I:
1000 FH
MRB 9
325300-710-801
MRB REFERENCE:
32.53.00/01
1
1
0.10 A330-200
0.10 POST 43442
(32-3030)
PRE 56814
(32-3234)
PRE 58794
OR
A330-200
POST 201082
(32-3246)
OR
A330-200F
PRE 56814
(32-3234)
PRE 58794
OR
A330-200F
POST 201082
(32-3246)
OR
A330-300
POST 43442
(32-3030)
PRE 56814
(32-3234)
PRE 58794
OR
A330-300
POST 201082
(32-3246)
OR
A330-800
POST 201082
(32-3246)
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-32
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
325300-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-900
POST 201082
(32-3246)
326100-01-1
210 LANDING GEAR INDICATING AND WARNING
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF LANDING GEAR INDICATION
CIRCUITS.
326100-02-1
210 LANDING GEAR INDICATING AND WARNING
E N D
SYSTEMS, APU AND POWER PLANT : LANDING GEAR
1
0.15 ALL
1
0.66 ALL
MRB REFERENCE:
32.30.00/06
AF
OPC
I:
72 MO
MRB 9
OPERATIONAL CHECK OF GROUND DOORS CLOSURE INHIBIT.
* * * * *
326100-710-801
323100-710-804
MRB REFERENCE:
32.30.00/10
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-32
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
331400-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 ANNUNCIATOR LIGHT TEST AND DIMMING
EL
OPC
I:
2000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF LIGHTS.
N
334800-01-1
REFERENCE
331400-710-801
MEN
1
M/H
APPLICABILITY
0.10 ALL
MRB REFERENCE:
23.81.00/01
24.20.00/04
27.90.00/13
31.50.00/01
31.50.00/02
33.14.00/01
34.13.00/01
34.14.00/01
34.48.00/01
34.52.00/01
35.20.02/06
140 ANTI-COLLISION/STROBE LIGHTING
EL
VCK
244
VISUAL CHECK OF NEOL (NEAR END OF LIFE) ACTIVATION ON
BEACON LIGHTS.
T: 16600 FH
NOTE
I:
800 FH
I:
2000 FH
MRB 9
334800-200-801
1
1
TBD POST 207615
TBD
MRB REFERENCE:
33.48.00/01
NOTE:
THRESHOLD:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
R
335100-01-1
200 CABIN EMERGENCY LIGHTING
EL
OPC
MRB 9
OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNITS BY
BITE-CHECK.
R
335100-02-1
210 CABIN EMERGENCY LIGHTING
EL
OPC
BATTERY CAPACITY CHECK VIA MCDU.
335100-710-801
1
0.15 POST 43069
(33-3004)
1
0.50 POST 43069
(33-3004)
MRB REFERENCE:
33.51.00/01
I:
CE
NOTE
MRB 9
335100-710-802
MRB REFERENCE:
33.51.00/02
NOTE:
PLANNING:
- AS AN ALTERNATIVE, TASK MAY BE ACCOMPLISHED BY
INSTALLATION OF SERVICEABLE BATTERIES
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
* * * * *
SYSTEMS, APU AND POWER PLANT : LIGHTS
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -33
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
335100-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
335100-03-1
R
335100-04-1
200 CABIN EMERGENCY LIGHTING
EL
OPC
210
OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM
AUTOMATIC CONTROL CIRCUIT AND MANUAL ACTIVATION FROM
BOTH CONTROL PANELS.
I: 24000 FH
200 CABIN EMERGENCY LIGHTING
I:
EL
FNC
MRB 9
CE
NOTE
MRB 9
335100-06-1
241FW
200 CABIN EMERGENCY LIGHTING
242FW
261FW
OPC
I:
2000 FH
MRB 9
OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNITS VIA
EPSU TEST PUSHBUTTON.
SYSTEMS, APU AND POWER PLANT : LIGHTS
335100-710-807
262FW
EL
0.25 ALL
0.25
1
0.60 A330-200
PRE 43069
(33-3004)
OR
A330-300
PRE 43069
(33-3004)
*
0.76
1
1.20 A330-200
PRE 43069
(33-3004)
OR
A330-300
PRE 43069
(33-3004)
MRB REFERENCE:
33.51.00/06
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
222DC
272FC
1
1
MRB REFERENCE:
33.51.00/03
REMOVE BATTERIES FOR CAPACITY CHECK.
ACCESS: 221DC
271FC
335100-710-803
335100-710-806
MRB REFERENCE:
33.51.00/05
REV. DATE: JUL 01/21
SECTION:
2-33
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
335100-07-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CABIN EMERGENCY LIGHTING
AF
OPC
I:
2000 FH
SOURCE
MRB 9
OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM
INCLUDING CHECK OF ALL CABIN LIGHTS AND SIGNS.
ACCESS: 831
N
335100-08-1
SYSTEMS, APU AND POWER PLANT : LIGHTS
335100-710-812
E N D
MEN
1
M/H
APPLICABILITY
TBD ALL
MRB REFERENCE:
33.51.00/07
841
*
220 CABIN EMERGENCY LIGHTING
EL
DIS
230
240 DISCARD OF EPSU BATTERY PACK.
250
260 NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
* * * * *
REFERENCE
I:
CE
NOTE
MRB 9
335100-920-801
MRB REFERENCE:
33.51.00/08
1
1
1
1
1
0.04
TBD ALL
TBD
TBD
TBD
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -33
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
341300-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 AIR DATA
RA
OPC
I:
48 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF PITOT PROBES HEATING (115 VAC)
AND ADR/AOA POWER SUPPLY (26 VAC) IN EMERGENCY
CONFIGURATION.
341300-03-1
121 AIR DATA
122
FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES.
RA
RST
R
341300-05-1
I:
24 MO
NOTE
I:
210 AIR DATA
I: 12000 FH
OPC
MRB 6
48 MO
MRB 6
341300-06-2
120 AIR DATA
AV
RST
341100-170-801
341100-790-801
MRB REFERENCE:
34.13.00/04
MRB 8
OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY.
R
M/H
APPLICABILITY
1
0.20 ALL
2
2
0.30 ALL
0.30
1
1
1
0.20 ALL
0.20
0.20
1
0.20 POST 53368
(34-3213)
OR
POST 204436
(31-3242)
1
0.35 ALL
1
1
0.25 ALL
0.25
MRB REFERENCE:
34.13.00/03
121 AIR DATA
RA
FNC
122
210 LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS.
RA
341100-710-804
MEN
MRB REFERENCE:
34.13.00/02
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
341300-04-1
REFERENCE
341300-710-806
MRB REFERENCE:
34.13.00/05
I:
1000 FH
MRB 6
CLEANING OF 1 OUT OF 3 PITOT PROBES.
341100-170-804
MRB REFERENCE:
34.13.00/06
NOTE:
TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3.
341300-07-2
120 AIR DATA
210
FUNCTIONAL TEST OF THE ADM ACCURACY.
SYSTEMS, APU AND POWER PLANT : NAVIGATION
AV
FNC
I:
48 MO
MRB 6
341300-720-802
MRB REFERENCE:
34.13.00/07
REV. DATE: JUL 01/21
SECTION:
2 -34
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
341400-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 INERTIAL REFERENCE SYSTEM
RA
OPC
I:
48 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF ATT/HDG SWITCHING.
341400-02-1
210 INERTIAL REFERENCE SYSTEM
RA
120 STANDBY ALTITUDE AND AIRSPEED
130
210 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS.
341100-710-802
MEN
M/H
APPLICABILITY
1
0.15 ALL
1
0.20 ALL
1
1
1
0.55 PRE 47244
0.55 (34-3120),
0.55 (34-3230),
(34-3267)
*
*
*
0.10
0.31
0.05
1
0.30 PRE 47244
(34-3120),
(34-3230),
(34-3267)
1
1
1
0.45 POST 47244
0.45 (34-3120),
0.45 (34-3230),
(34-3267)
MRB REFERENCE:
34.14.00/02
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF ADIRU 1, 2 AND 3 POWER SUPPLY IN
EMERGENCY CONFIGURATION.
342100-01-1
REFERENCE
AV
RST
341100-710-803
MRB REFERENCE:
34.14.00/03
I:
24 MO
NOTE
MRB 6
341100-170-803
MRB REFERENCE:
34.21.00/01
NOTE:
PLANNING:
- THIS TASK PRECLUDES TASK 342100-02-1.
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 821
132AZ
211BW
342100-02-1
132EG
210 STANDBY ALTITUDE AND AIRSPEED
AV
FNC
I:
48 MO
MRB 6
LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS.
R
342200-01-1
120 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)
130
210 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS.
AV
RST
MRB REFERENCE:
34.21.00/02
I:
24 MO
NOTE
MRB 6
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : NAVIGATION
342225-170-801
MRB REFERENCE:
34.22.20/01
NOTE:
PLANNING:
- THIS TASK PRECLUDES TASK 342200-02-1.
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
* * * * *
341100-790-802
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -34
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
342200-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
1.11
0.05
1
0.30 POST 47244
(34-3120),
(34-3230),
(34-3267)
1
1
0.20 POST 47244
0.20 (34-3120),
(34-3230),
(34-3267)
2
2.00 POST 44754
(34-3092),
(34-3236)
PRE 44950
(53-3115)
0.05 OR
POST 44100
(34-3065),
(34-3284),
(34-3312)
PRE 44950
(53-3115)
* * * * *
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 132AZ
211BW
342200-02-1
132EG
132LF
210 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)
AV
FNC
I:
48 MO
MRB 6
LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS.
R
342200-03-1
344100-01-1
120 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) AV
210
OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY.
OPC
110 WEATHER RADAR SYSTEM
FNC
RA
342225-790-801
MRB REFERENCE:
34.22.20/02
I:
2000 FH
MRB 8
342225-710-801
MRB REFERENCE:
34.22.20/03
I:
30 MO
MRB 9
RADIO ELECTRICAL TEST OF THE RADOME (FOR KEVLAR
RADOME WITH PWS ACTIVATED).
531511-760-802
MRB REFERENCE:
34.41.00/01
ACCESS: 110AL
344200-01-1
*
150 RADIO ALTIMETER
RA
DET
I:
36 MO
MRB 9
DETAILED INSPECTION AND OPERATIONAL CHECK OF THE
RADIO ALTIMETER FAN.
ACCESS: 152PW
SYSTEMS, APU AND POWER PLANT : NAVIGATION
344200-750-801
1
0.80 ALL
*
0.20
MRB REFERENCE:
34.42.00/01
152UW
REV. DATE: JUL 01/21
SECTION:
2 -34
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
344200-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
150 RADIO ALTIMETER
RA
RST
I:
6 MO
NOTE
SOURCE
MRB 6
CLEANING OF RADIO ALTIMETER ANTENNAS EXTERNAL
SURFACE.
REFERENCE
344211-615-801
MEN
M/H
APPLICABILITY
1
0.10 ALL
1
0.10 IF (E)GPWS
INSTALLED
1
0.10 IF T2CAS INSTALLED
2
0.40 IF T/TISS (OR
T3CAS) INSTALLED
1
0.20 POST 49769
(34-3117)
PRE 53522
(34-3154)&
(34-3243)
1
0.20 PRE 47245
PRE 50859
PRE 53622
(34-3252)
OR
PRE 47245
PRE 50859
MRB REFERENCE:
34.42.00/02
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
344800-01-1
210 TERRAIN AWARENESS AND WARNING SYSTEM
RA
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM.
344800-02-1
210 TERRAIN AWARENESS AND WARNING SYSTEM
RA
MRB REFERENCE:
34.48.00/02
OPC
I:
48 MO
MRB 9
BITE TEST OF THE T2CAS (TAWS PART).
344800-03-1
210 TERRAIN AWARENESS AND WARNING SYSTEM
RA
OPC
I:
48 MO
MRB 9
210 ATC MODE S (SELECT)
RA
210 AUTOMATIC DIRECTION FINDER (ADF)
OPC
I: 24000 FH
MRB 8
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : NAVIGATION
345200-720-802
MRB REFERENCE:
34.52.00/02
RA
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF ADF 1 IN EMERGENCY
CONFIGURATION.
* * * * *
347200-740-801
MRB REFERENCE:
34.48.00/02
OPERATIONAL CHECK OF THE REMOTE ATC SYSTEM.
345300-01-1
344300-740-802
MRB REFERENCE:
34.48.00/02
BITE TEST OF THE T/TISS (TAWS PART).
345200-02-1
344800-740-801
345700-710-801
MRB REFERENCE:
34.53.00/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-34
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
345300-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 54662
OR
POST 50860
(34-3313)
PRE 53622
(34-3252)
OR
POST 50860
(34-3313)
POST 54662
345500-01-1
210 VOR/MARKER
RA
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF VOR 1 IN EMERGENCY
CONFIGURATION.
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : NAVIGATION
345700-710-802
MRB REFERENCE:
34.55.00/01
1
0.20 PRE 53622
(34-3252)
OR
POST 54662
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -34
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351000-19-1
R
351000-20-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
122 CREW OXYGEN
210
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH.
AF
122 CREW OXYGEN
AF
FNC
I:
72 MO
SOURCE
MRB 9
121 CREW OXYGEN
351300-720-801
MEN
DIS
I:
240 MO
MRB 6
AF
351112-920-801
I:
CE
NOTE
MRB 6,9
REMOVE OXYGEN CYLINDER FOR IN SHOP HYDROSTATIC TEST
AND FUNCTIONAL CHECK OF OXYGEN CYLINDER PRESSURE
GAUGE.
351141-750-801
1
0.50 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
1
0.20 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
*
0.05
1
0.10 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
35.10.00/04
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 811
351200-03-1
210 CREW OXYGEN
AF
OPC
I:
24 MO
NOTE
MRB 8
OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK.
MRB REFERENCE:
35.10.00/03
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
SYSTEMS, APU AND POWER PLANT : OXYGEN
351241-710-801
REV. DATE: JUL 01/21
SECTION:
2 -35
APPLICABILITY
0.50 A330-200
0.50 OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
35.10.00/20
FNC
M/H
1
1
MRB REFERENCE:
35.10.00/19
DISCARD CREW OXYGEN LOW PRESSURE SUPPLY HOSES
(FLEXIBLE HOSES).
351141-01-1
REFERENCE
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351200-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 CREW OXYGEN
AF
DET
I:
24 MO
SOURCE
MRB 8
DETAILED INSPECTION OF CREW OXYGEN MASKS (OUT OF BOX
WITH HARNESS INFLATED).
351200-06-1
122 CREW OXYGEN
AF
FNC
REFERENCE
351241-200-803
MEN
REMOVE PRESSURE REDUCER TRANSMITTER FOR IN SHOP
FUNCTIONAL CHECK.
72 MO
NOTE
MRB 8
36 MO
OR
6500 FH
MRB 8
72 MO
MRB 8
351315-920-801
0.20 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
1
0.30 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
1
1
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
A330-900
1
1
0.15 A330-200F
0.15
*
0.20
1
1
0.10 A330-200F
0.10
*
0.20
1
1
0.30 A330-200F
0.30
MRB REFERENCE:
35.10.00/06
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
351200-07-1
351200-08-1
122 CREW OXYGEN
AF
FNC
210
CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN
FILL PANEL AND GAUGES ON OXYGEN CYLINDERS.
I:
132 CREW OXYGEN
AF
210
OPERATIONAL CHECK OF OXYGEN CYLINDER HANDVALVE
SWITCHES.
I:
OPC
351000-200-806
MRB REFERENCE:
35.10.00/07
352300-710-818
MRB REFERENCE:
35.10.00/08
ACCESS: 132NX
351200-09-1
132 CREW OXYGEN
210
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH.
AF
FNC
I:
72 MO
OR
40000 FH
MRB 9
MRB REFERENCE:
35.10.00/09
ACCESS: 132NX
351200-10-1
132 CREW OXYGEN
200
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
AF
C O N T I N U E D
FNC
I:
72 MO
352300-720-812
MRB 8
352200-720-803
APPLICABILITY
1
MRB REFERENCE:
35.10.00/01
I:
M/H
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351200-10-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
1
0.30
*
0.20
1
1
0.20 A330-200F
0.20
*
0.20
1
1
0.15 A330-200F
0.15
1
0.10 A330-200F
1
1
0.30 A330-200F
0.30
*
0.20
* * * * *
210 FUNCTIONAL CHECK OF OXYGEN SYSTEM PRESSURE HOLDING
CHARACTERISTICS AND OPERATIONAL CHECK OF BLEED/VENT
VALVE.
MRB REFERENCE:
35.10.00/10
NOTE:
ETOPS RELEVANT
ACCESS: 132NX
351200-11-1
132 CREW OXYGEN
AF
210
FUNCTIONAL CHECK OF ALTITUDE PRESSURE SWITCH.
FNC
I:
72 MO
OR
15000 FH
CMR**
MRB 9
ACCESS: 132NX
351200-12-1
352300-720-813
CMR REFERENCE:
351000-00001-1-C
MRB REFERENCE:
35.10.00/11
200 CREW OXYGEN
AF
OPC
210
OPERATIONAL CHECK OF OXYGEN MANUAL ACTIVATION AND
CONTAINER DOOR OPENING.
I:
24 MO
MRB 8
352100-710-808
MRB REFERENCE:
35.10.00/12
NOTE:
ETOPS RELEVANT
351200-13-1
210 CREW OXYGEN
AF
OPC
I:
72 MO
MRB 8
OPERATIONAL CHECK OF THE CABIN OXYGEN SUPPLY OFF
INDICATION AND MONITORING FUNCTION.
351200-14-1
132 CREW OXYGEN
AF
OPC
200
OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICE
IN OXYGEN MASK CONTAINERS.
352300-710-817
MRB REFERENCE:
35.10.00/13
I:
60 MO
MRB 8
352200-710-807
MRB REFERENCE:
35.10.00/14
NOTE:
ETOPS RELEVANT
ACCESS: 132NX
SYSTEMS, APU AND POWER PLANT : OXYGEN
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351200-15-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CREW OXYGEN
AF
DET
I:
72 MO
SOURCE
MRB 8
DETAILED INSPECTION OF CONTINOUS FLOW OXYGEN MASKS.
132 CREW OXYGEN
AF
OPC
210
OPERATIONAL CHECK OF CABIN OXYGEN SYSTEM CONTROL AND
REDUNDANCY FUNCTIONS.
352100-200-802
MEN
M/H
APPLICABILITY
1
0.70 A330-200F
1
1
0.20 A330-200F
0.20
*
0.20
1
0.30 A330-200F
*
0.20
1
1
0.10 A330-200F
0.10
*
0.20
1
0.75 A330-200F
MRB REFERENCE:
35.10.00/15
NOTE:
ETOPS RELEVANT
351200-16-1
REFERENCE
I:
48 MO
MRB 8
352300-710-819
MRB REFERENCE:
35.10.00/16
NOTE:
ETOPS RELEVANT
ACCESS: 132NX
351200-17-1
132 CREW OXYGEN
AF
FNC
I:
REMOVE PRESSURE REDUCER TRANSMITTER FOR IN SHOP
FUNCTIONAL CHECK.
CE
NOTE
MRB 6,8
352300-720-811
MRB REFERENCE:
35.10.00/17
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 132NX
351200-18-1
132 CREW OXYGEN
AF
FNC
210
CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN
FILL PANEL AND GAUGES ON OXYGEN CYLINDERS.
I:
2000 FH
MRB 8
351000-200-804
MRB REFERENCE:
35.10.00/18
ACCESS: 132NX
351200-21-1
120 CREW OXYGEN
AF
FNC
I:
60 MO
NOTE
MRB 6,9
REMOVE OXYGEN CYLINDER FOR IN SHOP HYDROSTATIC TEST
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
351141-750-803
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351200-21-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.05
1
1
0.05 A330-200F
0.05
1
1
0.67 A330-200F
0.67
1
1
0.10 A330-200F
0.10
1
0.50 A330-200
OR
A330-300
OR
A330-800
* * * * *
AND FUNCTIONAL CHECK OF CYLINDER PRESSURE GAUGE.
35.10.00/21
NOTE:
- ETOPS RELEVANT
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 811
351200-22-1
211 CREW OXYGEN
AF
OPC
212
OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK.
I:
24 MO
MRB 8
351241-710-806
MRB REFERENCE:
35.10.00/22
NOTE:
ETOPS RELEVANT
351200-23-1
211 CREW OXYGEN
AF
FNC
212
REMOVE OXYGEN MASK REGULATOR FOR IN SHOP FUNCTIONAL
CHECK.
I:
72 MO
NOTE
MRB 8
351241-720-803
MRB REFERENCE:
35.10.00/23
NOTE:
- ETOPS RELEVANT
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
351200-24-1
211 CREW OXYGEN
AF
DET
212
DETAILED INSPECTION OF CREW OXYGEN MASKS (OUT OF BOX
WITH HARNESS INFLATED).
I:
24 MO
MRB 8
351241-200-807
MRB REFERENCE:
35.10.00/24
NOTE:
ETOPS RELEVANT
351315-01-1
210 CREW OXYGEN MASK REGULATOR
AF
FNC
I:
72 MO
NOTE
MRB 8
REMOVE OXYGEN MASK REGULATOR FOR IN SHOP FUNCTIONAL
CHECK.
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
351241-720-801
MRB REFERENCE:
35.10.00/05
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
351315-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
200 PASSENGER OXYGEN (CHEMICAL)
OR
A330-900
AF
OPC
I:
4 C
MRB 9
OPERATIONAL CHECK OF IN SEAT POWER SUPPLY
INTERRUPTION.
352001-07-1
APPLICABILITY
* * * * *
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
352001-06-1
M/H
352300-710-808
1
0.25 IF PASSENGER OXYGEN
SYSTEM (CHEMICAL)
AND INSEAT POWER
SUPPLY INSTALLED
1
1
0.10 IF CREW REST ROOM
0.10 WITH CHEMICAL
OXYGEN INSTALLED
1
1
0.50 IF CREW REST ROOM
0.50 WITH CHEMICAL
OXYGEN INSTALLED
1
0.50 A330-200
POST 203608
(25-3583),
MRB REFERENCE:
35.20.01/06
100 PASSENGER OXYGEN (CHEMICAL)
AF
VCK
200
VISUAL CHECK OF CRR CHEMICAL OXYGEN GENERATORS FOR
SIGNS OF DISCHARGE.
I:
6 YE
NOTE
MRB 8
352100-210-804
MRB REFERENCE:
35.20.01/07
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
352001-08-1
100 PASSENGER OXYGEN (CHEMICAL)
200
DISCARD CRR CHEMICAL OXYGEN GENERATORS.
AF
DIS
I:
CE
NOTE
MRB 8
MRB REFERENCE:
35.20.01/08
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED.
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
352001-09-1
200 PASSENGER OXYGEN (CHEMICAL)
AF
DIS
I:
25 YE
NOTE
MRB 8
DISCARD GASEOUS LAVATORY OXYGEN CONTAINER.
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
352142-920-802
352141-920-801
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352001-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
35.20.01/09
SYSTEMS, APU AND POWER PLANT : OXYGEN
M/H
APPLICABILITY
* * * * *
(25-3591),
(25-3593),
(25-3596),
(25-3598),
(25-3602),
(25-3603),
(25-3605),
(25-3609),
(25-3611)
OR
A330-200
POST 203609
(25-3588),
(25-3595),
(25-3600),
(25-3601),
(25-3607),
(25-3611),
(25-3612),
(25-3691)
OR
A330-300
POST 203608
(25-3583),
(25-3591),
(25-3593),
(25-3596),
(25-3598),
(25-3602),
(25-3603),
(25-3605),
(25-3609),
(25-3611),
(25-3704)
OR
A330-300
POST 203609
(25-3588),
(25-3595),
(25-3600),
(25-3601),
(25-3607),
(25-3611),
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
* * * * *
MEN
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352001-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
(25-3612)
OR
A330-800
POST 203608
OR
A330-800
POST 203609
OR
A330-900
POST 203608
OR
A330-900
POST 203609
352002-14-1
200 PASSENGER OXYGEN (GASEOUS)
AF
OPC
I:
4 C
MRB 9
OPERATIONAL CHECK OF IN SEAT POWER SUPPLY
INTERRUPTION.
352002-15-1
130 PASSENGER OXYGEN (GASEOUS)
AF
FNC
I: 40000 FH
OR
CE
NOTE
CMR**
MRB 9
352002-16-1
0.30 A330-200
POST 52485
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
0.55
MRB REFERENCE:
35.20.02/15
AF
FNC
I: 16500 FH
OR
CE
NOTE
CMR**
MRB 8
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
C O N T I N U E D
1
*
REMOVE PRESSURE REGULATOR FOR PRESSURE REGULATING AND
LEAKAGE TEST IN THE SHOP.
SYSTEMS, APU AND POWER PLANT : OXYGEN
352300-720-806
132UW
130 PASSENGER OXYGEN (GASEOUS)
* * * * *
0.75 IF PASSENGER OXYGEN
SYSTEM (GASEOUS)
AND INSEAT POWER
SUPPLY INSTALLED
CMR REFERENCE:
352002-00002-1-C
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
132QW
1
MRB REFERENCE:
35.20.02/14
REMOVE PRESSURE RELIEF VALVE FOR IN SHOP FUNCTIONAL
CHECK.
ACCESS: 132FX
352300-710-807
352300-780-803
CMR REFERENCE:
352002-00003-1-C
MRB REFERENCE:
35.20.02/16
1
0.50 A330-200
POST 52485
OR
A330-300
POST 56322
OR
A330-800
POST 52485
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352002-16-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
* * * * *
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 132FX
352002-17-1
132QW
OR
A330-900
POST 56322
132UW
130 PASSENGER OXYGEN (GASEOUS)
200
OPERATIONAL CHECK OF CYLINDER VALVE SWITCH.
AF
OPC
I:
4 C
MRB 9
352300-710-809
0.55
1
1
0.15 A330-200
0.15 POST 52485
OR
A330-300
5.00 POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
*
132 PASSENGER OXYGEN (GASEOUS)
AF
FNC
REMOVE PRESSURE REDUCER FOR IN SHOP FUNCTIONAL CHECK.
I: 15000 FH
OR
CE
NOTE
CMR**
MRB 8
352300-720-815
AF
FNC
0.80 A330-200
POST 40257
PRE 49144
OR
A330-300
POST 40257
PRE 49144
*
0.20
1
0.80 A330-200
POST 40257
POST 49144
OR
A330-200
POST 52485
OR
A330-300
POST 40257
POST 49144
0.20 OR
MRB REFERENCE:
35.20.02/18
ACCESS: 132NX
132 PASSENGER OXYGEN (GASEOUS)
1
CMR REFERENCE:
352002-00004-1-C
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
352002-18-2
*
MRB REFERENCE:
35.20.02/17
PREP.: SIDEWALL LININGS Z130;
352002-18-1
I:
CE
NOTE
MRB 8
REMOVE PRESSURE REDUCER FOR IN SHOP FUNCTIONAL CHECK.
352300-720-815
MRB REFERENCE:
35.20.02/18
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 132NX
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
APPLICABILITY
*
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352002-18-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
352002-19-1
132 PASSENGER OXYGEN (GASEOUS)
AF
OPC
I:
72 MO
MRB 8
OPERATIONAL CHECK OF CHECK VALVES FOR DEPLETION
PREVENTION.
352002-20-1
132 PASSENGER OXYGEN (GASEOUS)
AF
1
0.50 A330-200
POST 203799
(35-3042)
OR
A330-300
POST 203799
(35-3042)
OR
A330-800
POST 203799
(35-3042)
OR
A330-900
POST 203799
(35-3042)
1
1.50 A330-200
POST 203799
(35-3042)
OR
A330-300
POST 203799
(35-3042)
OR
A330-800
POST 203799
(35-3042)
OR
A330-900
POST 203799
(35-3042)
MRB REFERENCE:
35.20.02/19
FNC
I:
180 MO
MRB 9
REMOVE CHECK VALVES FOR DEPLETION PREVENTION FOR IN
SHOP FUNCTIONAL CHECK.
SYSTEMS, APU AND POWER PLANT : OXYGEN
352100-710-809
352100-720-804
MRB REFERENCE:
35.20.02/20
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
352002-21-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
132 PASSENGER OXYGEN (GASEOUS)
AF
DIS
I:
240 MO
SOURCE
MRB 6,9
DISCARD PASSENGER OXYGEN INTERMEDIATE PRESSURE SUPPLY
HOSES (FLEXIBLE HOSES).
352002-22-1
352002-23-1
132 PASSENGER OXYGEN (GASEOUS)
210
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH.
AF
200 PASSENGER OXYGEN (GASEOUS)
AF
FNC
REFERENCE
352112-920-801
I:
72 MO
MRB 9
352300-720-817
REMOVE DIFFERENTIAL PRESSURE SWITCH FOR IN SHOP
FUNCTIONAL CHECK.
I:
144 MO
NOTE
MRB 8
352300-720-816
MRB REFERENCE:
35.20.02/23
NOTE:
INTERVAL:
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
M/H
APPLICABILITY
1
2.25 A330-200
POST 40257
OR
A330-200
POST 52485
OR
A330-300
POST 40257
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
1
1
2.00 A330-200
2.00 POST 40257
OR
A330-200
POST 52485
OR
A330-300
POST 40257
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
1
0.50 A330-200
POST 40257
OR
A330-200
POST 52485
OR
A330-300
MRB REFERENCE:
35.20.02/21
MRB REFERENCE:
35.20.02/22
FNC
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352002-23-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
ACCESS: 252ZW
*
146 PASSENGER OXYGEN (GASEOUS)
AF
152
250 REMOVE RISER LINE SHUT OFF VALVES FOR FUNCTIONAL
264 CHECK.
FNC
I:
CE
NOTE
MRB 8
352200-720-804
MRB REFERENCE:
35.20.02/24
POST 40257
OR
0.10 A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
1
1
1
1
1.18
1.18
1.18
1.18
*
0.21
1
1
0.20 A330-200
0.20 POST 40257
OR
A330-300
0.31 POST 40257
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 251CC
352002-25-1
252NW
252WW
132 PASSENGER GASEOUS OXYGEN DISTRIBUTION
AF
OPC
200
OPERATIONAL CHECK OF SYSTEM SHUT-OFF VALVES OPENING.
ACCESS: 132AZ
352100-01-1
251HC
132QW
I:
18 MO
MRB 8
MRB REFERENCE:
35.20.02/25
*
AF
OPC
I:
6 YE
MRB 8
OPERATIONAL CHECK OF MANUAL MASK RELEASE.
SYSTEMS, APU AND POWER PLANT : OXYGEN
352200-710-801
821
200 PASSENGER OXYGEN ( CHEMICAL )
* * * * *
APPLICABILITY
* * * * *
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
352002-24-1
M/H
C O N T I N U E D
352100-710-804
MRB REFERENCE:
35.20.01/03
1
A330-200
POST 52485
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
0.50 A330-200
PRE 40257
PRE 52485
OR
A330-300
PRE 40257
PRE 56322
OR
A330-800
PRE 52485
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352100-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-900
PRE 56322
352100-02-1
120 PASSENGER OXYGEN ( CHEMICAL )
200
210 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE.
AF
FNC
I:
4 C
MRB 9
MRB REFERENCE:
35.20.01/01
ACCESS: 132AZ
352100-03-1
200 PASSENGER OXYGEN ( CHEMICAL )
352100-720-801
AF
VCK
I:
6 YE
MRB 8
VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS
OF DISCHARGE.
352100-210-802
AF
DET
I:
4 C
NOTE
MRB 9
DETAILED INSPECTION OF OXYGEN MASKS.
352100-210-803
MRB REFERENCE:
35.20.01/02
NOTE:
INTERVAL:
- TASK IS ALSO APPLICABLE FOR CRR(U). INTERVAL 6 YE
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
1
*
200 PASSENGER OXYGEN (CHEMICAL)
* * * * *
*
MRB REFERENCE:
35.20.01/04
PREP.: MASKS OUT OF CONTAINER;
352100-04-1
1
1
1
1
0.60 A330-200
0.60 PRE 40257
0.60 PRE 52485
OR
0.01 A330-300
PRE 40257
PRE 56322
OR
A330-800
PRE 52485
OR
A330-900
PRE 56322
5.00 A330-200
PRE 40257
PRE 52485
OR
A330-300
10.00 PRE 40257
PRE 56322
OR
A330-800
PRE 52485
OR
A330-900
PRE 56322
8.00 A330-200
PRE 40257
PRE 52485
OR
A330-300
PRE 40257
PRE 56322
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
200 PASSENGER OXYGEN (GASEOUS)
AF
DET
I:
DETAILED INSPECTION OF OXYGEN MASK ASSEMBLIES.
6 YE
OR
12500 FH
CMR**
MRB 8
PREP.: MASKS OUT OF CONTAINERS;
352100-04-3
352100-210-803
200 PASSENGER OXYGEN (GASEOUS)
AF
DET
I:
6 YE
MRB 8
352100-210-803
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
FNC
I:
24 MO
MRB 8
352300-720-802
MRB REFERENCE:
35.20.02/03
132UW
C O N T I N U E D
1
8.00 A330-200
POST 40257
PRE 49144
OR
10.00 A330-300
POST 40257
PRE 49144
*
1
*
120 PASSENGER OXYGEN (GASEOUS)
AF
130
200 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION.
132QW
10.00 A330-800
PRE 52485
OR
A330-900
PRE 56322
MRB REFERENCE:
35.20.02/10
PREP.: MASKS OUT OF CONTAINERS;
ACCESS: 132FX
262NC
APPLICABILITY
*
CMR REFERENCE:
352002-00007-1-C
MRB REFERENCE:
35.20.02/10
DETAILED INSPECTION OF OXYGEN MASK ASSEMBLIES.
352100-05-1
M/H
* * * * *
PREP.: MASKS OUT OF CONTAINER;
352100-04-2
MEN
1
1
1
*
*
8.00 A330-200
POST 40257
POST 49144
OR
10.00 A330-200
POST 52485
OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
0.25 A330-200
0.25 POST 40257
0.25 POST 49144
OR
0.55 A330-200
0.04 POST 52485
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352100-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
352100-05-2
120 PASSENGER OXYGEN (GASEOUS)
AF
130
200 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION.
ACCESS: 132FX
132QW
262NC
352100-06-1
FNC
I:
24 MO
OR
9500 FH
CMR**
MRB 8
CMR REFERENCE:
352002-00009-1-C
132UW
200 PASSENGER OXYGEN (GASEOUS)
AF
OPC
I:
60 MO
MRB 8
OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICES
IN OXYGEN MASK CONTAINERS.
R
352142-01-1
352300-720-802
1
1
1
MRB REFERENCE:
35.20.02/03
*
*
*
352100-720-802
1
MRB REFERENCE:
35.20.02/11
PREP.: MASKS OUT OF CONTAINERS;
*
ACCESS: 132FX
*
132QW
132UW
262NC
200 PASSENGER OXYGEN (CHEMICAL)
AF
DIS
I:
CE
NOTE
MRB 8
DISCARD CHEMICAL OXYGEN GENERATORS.
MRB REFERENCE:
35.20.01/05
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 3
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
352142-920-801
1
0.25 A330-200
0.25 POST 40257
0.25 PRE 49144
OR
0.35 A330-300
0.20 POST 40257
0.04 PRE 49144
18.00 A330-200
POST 40257
OR
A330-300
POST 40257
10.00
0.59
16.00 A330-200
PRE 40257
PRE 52485
OR
A330-300
PRE 40257
PRE 56322
OR
A330-900
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352142-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
10.00
1
16.00 A330-800
PRE 52485
*
10.00
* * * * *
PRE
PREP.: MASKS OUT OF CONTAINER;
N
352142-01-2
200 PASSENGER OXYGEN (CHEMICAL)
AF
DIS
T:
10 YE
NOTE
I:
10 YE
NOTE
MRB 8
SEMR
DISCARD CHEMICAL OXYGEN GENERATORS.
NOTE:
- NO SHORT-TERM EXTENSION IS ALLOWED
- THE THRESHOLD/INTERVAL OF 10 YE IS THE TIME SINCE
ITS MANUFACTURING DATE
- XX REPRESENTS ANY NUMERICAL VALUE
352142-920-801
MRB REFERENCE:
35.20.01/05
SEMR REFERENCE:
352001-00001-1-E
PREP.: MASKS OUT OF CONTAINER;
352151-01-1
130 PASSENGER OXYGEN (GASEOUS)
AF
FNC
I:
REMOVE OXYGEN CYLINDER FOR IN SHOP HYDROSTATIC TEST.
60 MO
NOTE
MRB 6
352100-790-801
1
MRB REFERENCE:
35.20.02/01
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
ACCESS: 132FX
352200-01-1
132QW
132UW
*
130 PASSENGER GASEOUS OXYGEN DISTRIBUTION
AF
OPC
210
OPERATIONAL CHECK OF THE PRESSURE REGULATORS OPENING.
ACCESS: 132FX
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
132QW
I:
24 MO
MRB 8
352200-710-801
MRB REFERENCE:
35.20.02/04
132UW
C O N T I N U E D
56322
1
1
*
2.00 A330-200
POST 40257
OR
A330-200
POST 52485
OR
A330-300
POST 40257
0.55 OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
0.20 A330-200
0.20 POST 52485
OR
A330-300
0.55 POST 56322
OR
A330-800
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-35
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352200-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 52485
OR
A330-900
POST 56322
352200-02-1
130 PASSENGER GASEOUS OXYGEN DISTRIBUTION
AF
210
OPERATIONAL CHECK OF MANUAL SYSTEM OPERATION.
ACCESS: 132FX
352200-02-2
132QW
I:
24 MO
MRB 8
MRB REFERENCE:
35.20.02/05
OPC
I:
24 MO
OR
9500 FH
CMR**
MRB 8
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
352200-710-802
132UW
MRB REFERENCE:
35.20.02/05
AF
VCK
I:
60 MO
MRB 8
352200-200-801
*
1
MRB REFERENCE:
35.20.02/09
132UW
C O N T I N U E D
1
1
CMR REFERENCE:
352002-00010-1-C
VISUAL CHECK OF OVERBOARD DISCHARGE LINE FOR DAMAGE.
132QW
1
1
*
130 PASSENGER GASEOUS OXYG DISTRIBUTION
ACCESS: 132FX
352200-710-802
132UW
130 PASSENGER GASEOUS OXYGEN DISTRIBUTION
AF
210
OPERATIONAL CHECK OF MANUAL SYSTEM OPERATION.
ACCESS: 132FX
352200-05-1
132QW
OPC
*
0.20 A330-200
0.20 POST 40257
POST 49144
OR
0.55 A330-200
POST 52485
OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
0.20 A330-200
0.20 POST 40257
PRE 49144
OR
0.55 A330-300
POST 40257
PRE 49144
0.20 A330-200
POST 40257
OR
A330-200
0.55 POST 52485
OR
A330-300
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352200-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 40257
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
352200-06-1
200 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
OPC
210
OPERATIONAL CHECK OXYGEN CONTAINER OPENING AND VENT
FUNCTION OF BLEED/VENT VALVE.
ACCESS: 132FX
352200-06-2
132QW
132UW
261NC
SYSTEMS, APU AND POWER PLANT : OXYGEN
132QW
132UW
261NC
30 MO
OR
12500 FH
CMR**
MRB 8
I:
30 MO
352200-710-805
1
1
CMR REFERENCE:
352002-00005-1-C
271AC
200 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
OPC
210
OPERATIONAL CHECK OXYGEN CONTAINER OPENING AND VENT
FUNCTION OF BLEED/VENT VALVE.
ACCESS: 132FX
I:
MRB 8
MRB REFERENCE:
35.20.02/07
*
352200-710-805
1
1
MRB REFERENCE:
35.20.02/07
271AC
*
REV. DATE: JUL 01/21
SECTION:
2-35
0.50 A330-200
0.50 POST 40257
PRE 49144
OR
A330-300
0.64 POST 40257
PRE 49144
0.50 A330-200
0.50 POST 40257
POST 49144
OR
A330-200
0.64 POST 52485
OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352200-07-1
ZONE
130 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
OPC
200
210 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM.
ACCESS: 132FX
261UW
352200-07-2
132QW
CMR**
MRB 8
352200-710-803
CMR REFERENCE:
352002-00001-2-C
132QW
I:
60 MO
OR
15000 FH
CMR**
MRB 8
132UW
I:
60 MO
MRB 8
CMR REFERENCE:
352002-00001-1-C
AF
FNC
352200-710-803
MRB REFERENCE:
35.20.02/13
132UW
C O N T I N U E D
352200-710-803
MRB REFERENCE:
35.20.02/13
REMOVE RISER LINE SHUT-OFF VALVES FOR IN SHOP
FUNCTIONAL CHECK.
SYSTEMS, APU AND POWER PLANT : OXYGEN
60 MO
OR
9500 FH
REFERENCE
MRB REFERENCE:
35.20.02/13
200 PASSENGER GASEOUS OXYG DISTRIBUTION
* * * * *
I:
SOURCE
132UW
130 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
OPC
200
210 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM.
ACCESS: 132FX
261UW
352253-02-1
132QW
130 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
OPC
200
210 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM.
ACCESS: 132FX
261UW
352200-07-3
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
I:
60 MO
OR
25000 FH
CMR**
MRB 8
352200-720-802
CMR REFERENCE:
352002-00008-1-C
MEN
1
1
1
*
*
1
1
1
*
*
1
1
1
*
*
1
M/H
APPLICABILITY
0.70 A330-200
0.70 POST 40257
0.70 PRE 49144
OR
0.55 A330-300
0.10 POST 40257
PRE 49144
0.70 A330-200
0.70 POST 40257
0.70 POST 49144
OR
0.55 A330-200
0.10 POST 52485
POST 49144
OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
POST 49144
0.70 A330-200
0.70 POST 52485
0.70 PRE 49144
OR
0.55 A330-300
0.10 POST 56322
PRE 49144
OR
A330-800
POST 52485
OR
A330-900
POST 56322
3.00 A330-200
POST 40257
PRE 49144
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 19
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352253-02-1
ZONE
* * * * *
ACCESS: 132FX
252MC
352253-02-2
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
132QW
252NW
132UW
252WW
SOURCE
251CC
261PW
251HC
252EX
AF
FNC
I:
60 MO
MRB 8
REMOVE RISER LINE SHUT-OFF VALVES FOR IN SHOP
FUNCTIONAL CHECK.
352253-03-1
132UW
252WW
251CC
261PW
251HC
132QW
SYSTEMS, APU AND POWER PLANT : OXYGEN
132QW
*
352200-720-802
1
MRB REFERENCE:
35.20.02/12
*
FNC
I:
30 MO
OR
12500 FH
CMR**
MRB 8
FNC
I:
30 MO
352200-720-801
CMR REFERENCE:
352002-00006-1-C
132UW
132 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
200
210 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY
CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEM.
ACCESS: 132FX
262NC
MRB REFERENCE:
35.20.02/12
252EX
132 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
200
210 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY
CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEM.
ACCESS: 132FX
262NC
352253-03-2
132QW
252NW
MEN
M/H
APPLICABILITY
* * * * *
200 PASSENGER GASEOUS OXYG DISTRIBUTION
ACCESS: 132FX
252MC
REFERENCE
MRB 8
1
1
1
MRB REFERENCE:
35.20.02/08
*
*
352200-720-801
1
1
1
MRB REFERENCE:
35.20.02/08
132UW
*
*
REV. DATE: JUL 01/21
SECTION:
2-35
A330-300
0.88 POST 40257
PRE 49144
3.00 A330-200
POST 40257
POST 49144
OR
A330-300
0.88 POST 40257
POST 49144
0.50 A330-200
0.50 POST 40257
0.50 PRE 49144
OR
A330-300
0.55 POST 40257
0.04 PRE 49144
0.50 A330-200
0.50 POST 40257
0.50 POST 49144
OR
A330-200
0.55 POST 52485
0.04 OR
A330-300
POST 40257
POST 49144
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
PAGE 20
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
352300-01-1
ZONE
132 PASSENGER GASEOUS OXYG DISTRIBUTION
AF
210
CROSS-CHECK OF QUANTITY INDICATIONS ON ECAM
"DOOR/OXY"-PAGE, OXYGEN FILL PANEL AND OXYGEN
CYLINDERS.
ACCESS: 132FX
353000-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
132QW
FNC
I:
1400 FH
SOURCE
MRB 8
REFERENCE
352300-200-801
1
1
MRB REFERENCE:
35.20.02/02
132UW
200 PORTABLE OXYGEN
MEN
*
AF
VCK
I:
CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE.
1000 FH
NOTE
MRB 9
1000 FH
NOTE
MRB 9
353000-210-801
M/H
APPLICABILITY
0.10 A330-200
0.10 POST 40257
OR
A330-200
POST 52485
OR
0.55 A330-300
POST 40257
OR
A330-300
POST 56322
OR
A330-800
POST 52485
OR
A330-900
POST 56322
1
0.10 ALL
1
0.05 POST 46203
1
0.05 ALL
MRB REFERENCE:
35.30.00/02
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
353000-02-1
150 PORTABLE OXYGEN
AF
VCK
I:
CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE.
MRB REFERENCE:
35.30.00/02
NOTE:
PLANNING:
- PERFORMANCE OF TASK IS NOT REQUIRED BY MAINTENANCE
PERSONNEL IF ACCOMPLISHED AS PART OF A REGULATORY
AUTHORITY ACCEPTED/APPROVED FLIGHT CREW LIST
353100-01-1
210 FLIGHT CREW PORTABLE BREATHING EQPT
AF
VCK
I:
1000 FH
MRB 8
VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION
OF PROTECTIVE BREATHING EQUIPMENT.
SYSTEMS, APU AND POWER PLANT : OXYGEN
353000-210-804
353152-210-802
MRB REFERENCE:
35.30.00/01
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 21
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
353150-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 FLIGHT CREW PORTABLE BREATHING EQUIPT
AF
DIS
I:
120 MO
NOTE
SOURCE
MRB 8
DISCARD PROTECTIVE BREATHING EQUIPMENT.
200 PORTABLE OXYGEN
AF
GVI
I:
72 MO
MRB 9
GENERAL VISUAL INSPECTION OF OXYGEN CYLINDER
ATTACHMENT.
353200-02-1
353200-03-1
220 CABIN ATTENDANTS PORTABLE BREATHING EQ
AF
VCK
230
240 VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION
250 OF PROTECTIVE BREATHING EQUIPMENT.
260
270
I:
150 PORTABLE OXYGEN
I:
AF
150 FLIGHT CREW PORTABLE BREATHING EQUIPT
GVI
1000 FH
72 MO
MRB 8
MRB 9
APPLICABILITY
1
0.10 ALL
1
1.00 ALL
MRB REFERENCE:
35.30.00/01
1
1
1
1
1
1
0.03 ALL
0.03
0.03
0.03
0.03
0.03
353000-210-805
1
0.10 POST 46203
1
0.05 POST 46203
1
1
0.05 IF LDMCR INSTALLED
0.05
353000-210-803
353000-210-802
MRB REFERENCE:
35.30.00/05
CA
VCK
I:
1000 FH
MRB 8
VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION
OF PROTECTIVE BREATHING EQUIPMENT.
353200-05-1
M/H
MRB REFERENCE:
35.30.00/05
GENERAL VISUAL INSPECTION OF OXYGEN CYLINDER
ATTACHMENT.
353200-04-1
353152-920-801
MEN
MRB REFERENCE:
35.30.00/04
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353200-01-1
REFERENCE
150 FLIGHT CREW PORTABLE BREATHING EQUIPT
CA
VCK
160
VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION
OF PROTECTIVE BREATHING EQUIPMENT.
353000-210-806
MRB REFERENCE:
35.30.00/01
I:
1000 FH
NOTE
MRB 8
353000-210-807
MRB REFERENCE:
35.30.00/01
NOTE:
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 22
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
353200-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
353200-06-1
200 PORTABLE OXYGEN
AF
DET
I:
24 MO
MRB 9
DETAILED INSPECTION OF THE OXYGEN CONTINUOUS FLOW
MASK.
353200-07-1
200 PORTABLE OXYGEN
AF
353000-210-811
1
0.70 ALL
1
0.30 ALL
1
0.10 A330-200F
POST 200261
OR
A330-200
POST 58753
OR
A330-300
POST 58753
OR
A330-800
POST 58753
OR
A330-900
POST 58753
1
0.40 A330-200F
POST 200261
MRB REFERENCE:
35.30.00/06
FNC
I:
REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY WITH
CONTINUOUS FLOW MASK AND WITHOUT DEMAND/PRESSURE
DEMAND REGULATOR FOR IN SHOP HYDROSTATIC TEST AND
FUNCTIONAL CHECK OF OXYGEN REGULATOR.
60 MO
NOTE
MRB 9
60 MO
NOTE
MRB 8
353242-780-804
MRB REFERENCE:
35.30.00/07
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353200-08-1
200 PORTABLE OXYGEN
AF
FNC
I:
REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR IN SHOP
HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN
REGULATOR ASSEMBLY AND DEMAND/PRESSURE DEMAND
REGULATOR.
353242-780-805
MRB REFERENCE:
35.30.00/08
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353200-09-1
200 PORTABLE OXYGEN
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
AF
DET
I:
24 MO
MRB 8
353000-210-812
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 23
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
353200-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
MEN
200 PORTABLE OXYGEN
AF
MRB REFERENCE:
35.30.00/09
FNC
I:
60 MO
NOTE
MRB 9
REMOVE PORTABLE OXYGEN CYLINDER WITH FULL FLOW OUTLET
AND FULL FACE MASK ASSEMBLY FOR IN SHOP HYDROSTATIC
TEST AND FUNCTIONAL CHECK OF CYLINDER REGULATOR AND
FULL FACE MASK REGULATOR.
210 PORTABLE OXYGEN
353142-780-801
1
0.25 A330-200
POST 42516
OR
A330-300
POST 42516
OR
A330-800
POST 42516
OR
A330-900
POST 42516
1
0.40 A330-200
POST 42516
OR
A330-300
POST 42516
OR
A330-800
POST 42516
OR
A330-900
POST 42516
OR
A330-200
POST 58753
OR
A330-300
MRB REFERENCE:
35.30.00/10
AF
OPC
I:
24 MO
MRB 8
OPERATIONAL CHECK OF DEMAND / PRESSURE DEMAND
REGULATOR OR FULL FACE MASK REGULATOR.
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
APPLICABILITY
OR
A330-200
POST 42516
OR
A330-300
POST 42516
OR
A330-800
POST 42516
OR
A330-900
POST 42516
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353200-11-1
M/H
* * * * *
DETAILED INSPECTION OF FULL FACE MASK ASSEMBLY.
353200-10-1
REFERENCE
C O N T I N U E D
353142-710-801
MRB REFERENCE:
35.30.00/11
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 24
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
353200-11-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
POST 58753
OR
A330-800
POST 58753
OR
A330-900
POST 58753
OR
A330-200F
POST 200261
353250-01-1
200 CABIN ATTENDANTS PORTABLE BREATHING EQ
AF
DIS
I:
120 MO
NOTE
MRB 8
DISCARD PROTECTIVE BREATHING EQUIPMENT.
353252-920-801
1
0.30 ALL
1
0.10 POST 46203
1
1
0.10 IF LDMCR INSTALLED
0.10
MRB REFERENCE:
35.30.00/04
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353250-02-1
150 FLIGHT CREW PORTABLE BREATHING EQUIPT
CA
DIS
I:
DISCARD PROTECTIVE BREATHING EQUIPMENT.
120 MO
NOTE
MRB 8
120 MO
NOTE
MRB 8
353252-920-802
MRB REFERENCE:
35.30.00/04
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
353250-03-1
150 FLIGHT CREW PORTABLE BREATHING EQUIPT
160
DISCARD PROTECTIVE BREATHING EQUIPMENT.
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
C O N T I N U E D
CA
DIS
I:
353252-920-803
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 25
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
353250-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
35.30.00/04
NOTE:
PLANNING:
- FOR CRR(U) USERS ONLY: CRR(U) PART IS INCLUDED IN
THIS TASK. IF CRR(U) IS NOT FITTED WHEN TASK
BECOMES DUE, CRR(U) PART SHOULD BE PERFORMED WHEN
CRR(U) IS NEXT INSTALLED
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL
* * * * *
SYSTEMS, APU AND POWER PLANT : OXYGEN
E N D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -35
PAGE 26
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
360001-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 PNEUMATIC - GENERAL (NEO)
EN
DET
420
REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION.
I: 12000 FH
SOURCE
MRB 6
R
360001-02-1
416AR
426AR
417AL
427AL
361141-200-806
418AR
428AR
450 PNEUMATIC - GENERAL (NEO)
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
EN
FNC
I: 25000 FH
CMR*
MRB 9
361153-720-809
EN
FNC
I: 25000 FH
CMR*
MRB 9
NOTE:
ETOPS RELEVANT
361153-720-809
CMR REFERENCE:
360001-00001-1-C
450 PNEUMATIC - GENERAL (NEO)
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
EN
FNC
I: 20000 FH
CMP
CMR*
MRB 9
NOTE:
ETOPS RELEVANT
361153-720-809
2.42 A330-800
2.42 OR
A330-900
*
*
0.20
0.20
1
1
1.13 A330-800
1.13
*
*
0.50
0.35
1
1
1.13 NON-ETOPS
1.13 A330-900
*
*
0.50
0.35
1
1
1.13 ETOPS
1.13 A330-900
*
*
0.50
0.35
CMP REFERENCE:
36-2-0000-003
CMR REFERENCE:
360001-00001-1-C
ACCESS: 452CL
462CR
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
1
1
MRB REFERENCE:
36.00.01/02
ACCESS: 452CL
462CR
360001-02-3
APPLICABILITY
MRB REFERENCE:
36.00.01/02
ACCESS: 452CL
462CR
450 PNEUMATIC - GENERAL (NEO)
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
M/H
CMR REFERENCE:
360001-00001-1-C
NOTE:
ETOPS RELEVANT
360001-02-2
MEN
MRB REFERENCE:
36.00.01/01
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
REFERENCE
MRB REFERENCE:
36.00.01/02
REV. DATE: JUL 01/21
SECTION:
2 -36
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
360001-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 PNEUMATIC - GENERAL (NEO)
EN
OPC
I:
72 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF THE MANUAL CONTROL MODE FOR
CROSS BLEED VALVE.
REFERENCE
361200-710-805
MEN
M/H
APPLICABILITY
1
0.23 A330-800
OR
A330-900
1
1
0.15 A330-800
0.15 PRE 208995
OR
A330-900
PRE 208995
1
1
0.38 A330-800
0.38 PRE 208995
OR
A330-900
PRE 208995
1
0.10 GE
ETOPS
1
1
0.25 PW
0.25
*
*
0.06
0.02
1
1
0.25 TRENT 700
0.25
MRB REFERENCE:
36.00.01/03
NOTE:
ETOPS RELEVANT
R
R
360002-01-1
360002-02-1
361100-02-1
452 WING BELLOW
462
DETAILED INSPECTION OF THE WING BELLOW.
EN
452 WING BELLOW
462
DISCARD WING BELLOW.
EN
210 ENGINE BLEED
EN
DET
DIS
T:
1200 FC
I:
1200 FC
T: 20000 FC
SEMR
SEMR REFERENCE:
360001-00001-1-E
SEMR
I: 20000 FC
AIR SUPPLY
OPC
I:
36 MO
450 ENGINE AIR BLEED VALVE
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
EN
CMP
361100-04-1
361100-710-830
CMP REFERENCE:
36-2-0000-002
FNC
I: 20000 FH
CMP
MRB 9
361153-720-808
CMP REFERENCE:
36-2-0000-003
NOTE:
ETOPS RELEVANT
ACCESS: 416BR
461CL
361149-920-801
SEMR REFERENCE:
360001-00002-1-E
OPERATIONAL CHECK OF THE MANUAL BLEED SHUT OFF.
361100-03-1
361149-200-809
MRB REFERENCE:
36.00.00/03
426BR
461CR
451CL
451CR
450 ENGINE AIR BLEED VALVE
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
EN
FNC
I: 20000 FH
CMP
MRB 9
361153-720-808
CMP REFERENCE:
36-2-0000-003
NOTE:
* * * * *
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-36
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
361100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
361100-05-1
416AR
426AR
451CL
461CL
MRB REFERENCE:
36.00.00/03
451CR
461CR
210 ENGINE BLEED AIR SUPPLY
EN
OPC
I:
36 MO
CMP
OPERATIONAL CHECK OF MANUAL BLEED SHUT OFF.
361100-06-1
210 ENGINE BLEED AIR SUPPLY
361100-07-1
EN
OPC
I:
36 MO
CMP
EN
FNC
I: 20000 FH
CMP
MRB 9
0.12
0.12
1
0.10 PW
ETOPS
361100-710-830
1
0.10 RR
ETOPS
*
1.00
361153-720-808
1
1
0.25 GE
0.25
*
*
0.26
0.26
1
1
1.00 TRENT 700
1.00 IF P/N EB100904B
INSTALLED
OR
TRENT 700
IF P/N HTE450001-5
INSTALLED
0.20 OR
0.20 TRENT 700
IF P/N HTE450001-9
INSTALLED
CMP REFERENCE:
36-2-0000-003
416AR
426AR
451EL
461EL
451ER
461ER
I:
6400 FH
MRB 6
VSB
NOTE:
ETOPS RELEVANT
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
*
*
MRB REFERENCE:
36.00.00/03
410 ENGINE BLEED AIR SUPPLY
EN
DET
420
REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION.
ACCESS: 415AL
425AL
APPLICABILITY
CMP REFERENCE:
36-2-0000-002
NOTE:
ETOPS RELEVANT
361141-02-1
361100-710-830
462CL
450 ENGINE BLEED AIR VALVE
460
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
ACCESS: 415AL
425AL
M/H
CMP REFERENCE:
36-2-0000-002
OPERATIONAL CHECK OF MANUAL BLEED SHUT OFF.
ACCESS: 452CL
MEN
* * * * *
ETOPS RELEVANT
ACCESS: 415AL
425AL
REFERENCE
416AR
426AR
417AL
427AL
361141-200-804
VSB
RB211-36-E937
VSB
RB211-36-F770
MRB REFERENCE:
36.00.00/15
418AR
428AR
REV. DATE: JUL 01/21
SECTION:
2 -36
*
*
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
361141-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 ENGINE BLEED AIR SUPPLY
EN
DET
420
REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION.
I: 10000 FH
SOURCE
MRB 6
VSB
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
361141-03-1
416AR
426AR
417AL
427AL
REFERENCE
361141-200-804
VSB
RB211-36-E937
VSB
RB211-36-F770
MRB REFERENCE:
36.00.00/06
418AR
428AR
410 ENGINE BLEED AIR SUPPLY
EN
DET
420
REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION.
I:
6400 FH
MRB 6
361141-220-802
MEN
M/H
APPLICABILITY
1
1
1.00 TRENT 700
1.00 IF P/N AA1052-00
INSTALLED
*
*
0.20
0.20
1
1
0.40 GE
0.40
*
*
0.20
0.20
1
1
0.40 PW
0.40
*
*
0.06
0.06
1
1
1.00 A330-200
1.00 OR
A330-200F
OR
A330-300
0.85
0.85
MRB REFERENCE:
36.00.00/01
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
361141-04-1
416AR
426AR
417AL
427AL
418AR
428AR
410 ENGINE BLEED AIR SUPPLY
EN
DET
420
REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION.
I: 10000 FH
MRB 6
361141-220-801
MRB REFERENCE:
36.00.00/06
NOTE:
ETOPS RELEVANT
ACCESS: 415BL
425BL
361141-05-1
450 PNEUMATIC
EN
OPC
460
LEAK CHECK ON BLEED AIR DUCTING IN PYLON AREA BETWEEN
PRECOOLER AND PYLON-WING CONNECTION.
ACCESS: 452CL
462CL
361143-01-1
417AL
427AL
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
36 MO
MRB 9
361148-790-801
MRB REFERENCE:
36.00.00/16
452CR
462CR
*
*
450 ENGINE BLEED AIR SUPPLY
AF
RST
460
REMOVE THE FILTER OF THE FAN AIR VALVE THERMOSTAT FOR
* * * * *
I:
C O N T I N U E D
I:
6000 FH
NOTE
MRB 6
361143-100-801
MRB REFERENCE:
1
1
0.25 A330-200
0.25 OR
A330-200F
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -36
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
361143-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
* * * * *
CLEANING.
36.00.00/14
OR
A330-300
NOTE:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S
EXPERIENCE, A LESS OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED
- ETOPS RELEVANT
ACCESS: 452CL
462CR
361155-01-1
361155-01-2
210 ENGINE AIR BLEED SUPPLY
AV
OPC
I: 10000 FH
CMP
MRB 9
361100-710-830
OPERATIONAL CHECK OF CLOSING SIGNAL TO ISOLATION
SOLENOID FROM BLEED/FIRE PUSHBUTTON SWITCHES.
CMP REFERENCE:
36-2-0000-001
NOTE:
ETOPS RELEVANT
MRB REFERENCE:
36.00.00/04
210 ENGINE AIR BLEED SUPPLY
AV
OPC
I: 10000 FH
MRB 9
OPERATIONAL CHECK OF CLOSING SIGNAL TO ISOLATION
SOLENOID FROM BLEED/FIRE PUSHBUTTON SWITCHES.
361100-710-830
*
*
0.50
0.35
1
0.20 A330-200
ETOPS
OR
A330-200F
ETOPS
OR
A330-300
ETOPS
1
0.20 A330-200
NON-ETOPS
OR
A330-200F
NON-ETOPS
OR
A330-300
NON-ETOPS
1
0.10 A330-200
NON-ETOPS
OR
A330-200F
NON-ETOPS
OR
A330-300
NON-ETOPS
MRB REFERENCE:
36.00.00/04
NOTE:
ETOPS RELEVANT
361200-01-2
210 APU BLEED AIR VALVE AND CROSSBLEED
AV
OPC
I:
72 MO
MRB 9
OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE.
361200-710-802
MRB REFERENCE:
36.00.00/02
NOTE:
ETOPS RELEVANT
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
APPLICABILITY
REV. DATE: JUL 01/21
SECTION:
2-36
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
361200-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 APU BLEED AIR VALVE AND CROSSBLEED
AV
OPC
I:
OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE.
72 MO
OR
3600 FC
SOURCE
CMP
MRB 9
EN
DET
I:
8500 FH
MRB 9
REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION.
191HB
193 APU BLEED CHECK VALVE
DET
I: 10000 FC
MRB 9
REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION.
R
361251-01-5
1
*
I: 10000 FC
MRB 6,9
361251-200-803
191HB
REV. DATE: JUL 01/21
SECTION:
2 -36
0.75 A330-200
IF PN 2S7138
INSTALLED
OR
A330-200F
IF PN 2S7138
INSTALLED
2.30 OR
A330-300
IF PN 2S7138
INSTALLED
1
1
0.55 A330-800
0.55 OR
A330-900
*
2.30
MRB REFERENCE:
36.00.01/04
NOTE:
ETOPS RELEVANT
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
361251-200-803
191HB
191 PNEUMATIC - GENERAL (NEO)
EN
DET
193
REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION.
ACCESS: 191DZ
0.75 A330-200
IF PN 2S6674
INSTALLED
OR
A330-200F
IF PN 2S6674
INSTALLED
2.30 OR
A330-300
IF PN 2S6674
INSTALLED
MRB REFERENCE:
36.00.00/12
NOTE:
ETOPS RELEVANT
ACCESS: 191DZ
1
*
EN
APPLICABILITY
0.10 A330-200
ETOPS
OR
A330-200F
ETOPS
OR
A330-300
ETOPS
MRB REFERENCE:
36.00.00/07
NOTE:
ETOPS RELEVANT
361251-01-4
361251-200-803
M/H
1
MRB REFERENCE:
36.00.00/02
193 APU BLEED CHECK VALVE
ACCESS: 191DZ
361200-710-802
MEN
CMP REFERENCE:
36-2-0000-004
NOTE:
ETOPS RELEVANT
361251-01-3
REFERENCE
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
D
361251-01-6
ZONE
DESCRIPTION
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
************** TASK DELETED **************
* * * * *
SYSTEMS, APU AND POWER PLANT : PNEUMATIC
E N D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-36
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
381000-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
100 POTABLE WATER
200
DISINFECTION OF POTABLE WATER SYSTEM.
AF
RST
I:
3 MO
NOTE
SOURCE
MRB 8
R
381000-02-1
154AR
381000-670-801
164AR
200 POTABLE WATER
AF
DIS
I:
3 MO
NOTE
MRB 7,8
DISCARD WATER FILTER CARTRIDGE OF THE LAVATORIES.
381223-920-802
MRB REFERENCE:
38.10.00/02
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
MEN
M/H
APPLICABILITY
2
2
1.88 A330-200
1.88 OR
A330-300
OR
A330-800
OR
A330-900
*
0.04
1
1.50 A330-200
POST 42704
(25-3336)
OR
A330-300
POST 42704
(25-3336)
OR
A330-200
POST 46607
OR
A330-200
POST 49951
OR
A330-300
POST 49951
OR
A330-200
POST 57459
OR
A330-300
POST 57459
OR
A330-200
POST 200436
OR
A330-300
POST 200436
OR
A330-800
POST 207033
MRB REFERENCE:
38.10.00/01
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 133BL
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
381000-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-900
POST 207033
381000-03-1
200 POTABLE WATER
AF
DIS
I:
3 MO
NOTE
MRB 7,8
DISCARD WATER FILTER CARTRIDGE OF THE GALLEYS.
130 POTABLE WATER
200
DISINFECTION OF POTABLE WATER SYSTEM.
AF
RST
I:
3 MO
MRB 9
381000-670-806
MRB REFERENCE:
38.10.01/01
ACCESS: 133BL
381001-02-1
200 POTABLE WATER
AF
DIS
I:
3 MO
MRB 6,9
DISCARD WATER FILTER CARTRIDGE IN GALLEY.
381001-03-1
132 POTABLE WATER
AF
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
1.80 A330-200
WATER FILTER
CARTRIDGE OF
GALLEYS INSTALLED
OR
A330-300
WATER FILTER
CARTRIDGE OF
GALLEYS INSTALLED
OR
A330-800
WATER FILTER
CARTRIDGE OF
GALLEYS INSTALLED
OR
A330-900
WATER FILTER
CARTRIDGE OF
GALLEYS INSTALLED
1
1
0.60 A330-200F
0.60
*
0.02
381223-920-804
1
0.30 A330-200F
WATER FILTER
CARTRIDGE INSTALLED
1
0.25 A330-200F
MRB REFERENCE:
38.10.01/02
DIS
I: 40000 FH
MRB 9
DISCARD AIR MANIFOLD FILTER.
* * * * *
1
MRB REFERENCE:
38.10.00/03
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
381001-01-1
381223-920-803
384100-920-803
MRB REFERENCE:
38.10.01/03
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
381001-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
*
0.20
1
0.20 A330-200F
POST 200436
1
1
2.00 A330-200
2.00 OR
A330-300
OR
A330-800
OR
A330-900
PREP.: TOILET SYSTEM DISINFECTED;
TOILET SYSTEM DRAINED AND FLUSHED;
*
1.50
ACCESS: 161YW
*
0.17
1
0.40 A330-200
OR
A330-300
OR
A330-800
PRE 207472
OR
A330-900
PRE 207472
PREP.: TOILET SYSTEM DISINFECTED;
TOILET SYSTEM DRAINED AND FLUSHED;
*
1.50
ACCESS: 162ZW
*
0.02
* * * * *
C O N T I N U E
SOURCE
REFERENCE
* * * * *
ACCESS: 132WW
381001-06-1
200 POTABLE WATER
AF
DIS
I:
3 MO
MRB 6,9
DISCARD WATER FILTER CARTRIDGE IN LAVATORY.
383100-02-1
170 VACUUM TOILET SYSTEM
200
CORRECTIVE VACUUM WASTE LINE CLEANING.
381223-920-805
MRB REFERENCE:
38.10.01/06
AF
RST
I:
8500 FH
NOTE
MRB 6
383100-100-819
MRB REFERENCE:
38.31.00/16
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 383100-04-1
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383100-03-1
162ZW
170 TOILET SYSTEM
AF
DIS
I:
3200 FH
NOTE
MRB 9
DISCARD WATER SEPARATOR.
383147-100-801
MRB REFERENCE:
38.31.00/03
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
APPLICABILITY
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
383100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 TOILET SYSTEM
UT
RST
I:
350 FH
NOTE
SOURCE
MRB 6
REFERENCE
PREP.: TOILET SYSTEM DRAINED AND FLUSHED;
*
1.00
ACCESS: 171AL
*
0.01
1
4.00 A330-200
OR
A330-300
OR
A330-800
1.50 PRE 207472
OR
A330-900
0.18 PRE 207472
MRB REFERENCE:
38.31.00/04
170 TOILET SYSTEM
AF
RST
I:
CLEANING OF LIQUID LEVEL SENSORS, WASTE TANKS AND
WASTE DRAIN LINES.
383100-06-1
APPLICABILITY
1.00 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 383100-02-1
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383100-05-1
M/H
1
CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING
AGENT AND CRUSHED ICE.
383100-100-812
MEN
24 MO
OR
10000 FH
MRB 6,9
383100-100-808
MRB REFERENCE:
38.31.00/05
PREP.: TOILET SYSTEM DISINFECTED;
TOILET SYSTEM DRAINED AND FLUSHED;
*
ACCESS: 161YW
*
162ZW
171AL
170 TOILET SYSTEM
AF
RST
I:
3200 FH
NOTE
MRB 9
1
0.40 A330-200
OR
A330-300
OR
A330-800
PRE 207472
OR
A330-900
PRE 207472
PREP.: TOILET SYSTEM DISINFECTED;
TOILET SYSTEM DRAINED AND FLUSHED;
*
1.50
ACCESS: 162ZW
*
0.02
REMOVE FILTER OF POLAR CAP ASSY FOR IN SHOP CLEANING.
MRB REFERENCE:
38.31.00/06
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
383147-100-802
REV. DATE: JUL 01/21
SECTION:
2-38
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
383100-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
170 TOILET SYSTEM
AF
RST
I:
3200 FH
NOTE
SOURCE
MRB 6,9
REFERENCE
PREP.: TOILET SYSTEM DISINFECTED;
TOILET SYSTEM DRAINED AND FLUSHED;
*
1.50
ACCESS: 162ZW
*
0.07
1
0.50 A330-200
POST 55776
OR
A330-200
POST 201259
OR
A330-300
POST 55776
OR
A330-300
POST 201259
1
TBD A330-800
POST 207472
OR
A330-900
POST 207472
*
TBD
MRB REFERENCE:
38.31.00/07
823
200 TOILET SYSTEM
AF
OPC
I:
800 FH
NOTE
MRB 9
OPERATIONAL CHECK OF BIDET'S SPRAY NOZZLE.
383100-710-808
MRB REFERENCE:
38.31.00/13
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383100-14-1
APPLICABILITY
0.40 A330-200
OR
A330-300
OR
A330-800
PRE 207472
OR
A330-900
PRE 207472
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383100-13-1
M/H
1
CLEANING OF RINSE NOZZLES AND REFERENCE PRESSURE LINE
OF LIQUID LEVEL TRANSMITTER.
383157-100-802
MEN
170 TOILET SYSTEM
AF
DIS
I:
4000 FH
NOTE
MRB 6,9
DISCARD WASTE SEPARATOR EQUIPMENT (FILTER CARTRIDGE
AND CYCLONE).
383147-100-803
MRB REFERENCE:
38.31.00/14
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 161AZ
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
383100-15-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
170 TOILET SYSTEM
AF
RST
I: 18000 FH
NOTE
SOURCE
MRB 7
CLEANING OF WASTE TANK ASSEMBLY.
REFERENCE
383100-100-824
ACCESS: 161AZ
121 TOILET SYSTEM
AF
DET
I:
24 MO
MRB 9
DETAILED INSPECTION OF FLUSH NIPPLE CAP AND THE
OVERFLOW PORT CAP.
383100-220-801
121 TOILET SYSTEM
AF
DET
I:
24 MO
MRB 6
DETAILED INSPECTION OF WASTE CAP DRAIN VALVE.
383100-220-802
200 TOILET SYSTEM
AF
TBD A330-800
POST 207472
OR
A330-900
POST 207472
*
TBD
1
0.10 A330-200F
*
0.01
1
0.10 A330-200F
*
0.01
1
0.20 A330-200F
1
1.25 A330-200
POST 45556
OR
MRB REFERENCE:
38.31.01/02
ACCESS: 121FL
383101-03-1
APPLICABILITY
MRB REFERENCE:
38.31.01/01
ACCESS: 121EL
383101-02-1
M/H
1
MRB REFERENCE:
38.31.00/15
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383101-01-1
MEN
RST
I:
2000 FH
NOTE
MRB 9
CLEANING OF FILTER ELEMENT OF WASHBASIN SINK DRAIN
ASSEMBLY.
383200-100-805
MRB REFERENCE:
38.31.01/03
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
383242-01-1
200 WASTE WATER DRAIN
AF
RST
I:
600 FH
MRB 7
CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
383200-100-804
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
383242-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
M/H
APPLICABILITY
* * * * *
38.32.00/03
* * * * *
MEN
A330-200
POST 46554
OR
A330-200
POST 46582
(38-3038)
OR
A330-200
POST 49705
OR
A330-200
POST 50088
OR
A330-300
POST 45556
OR
A330-300
POST 46554
OR
A330-300
POST 46582
(38-3038)
OR
A330-300
POST 49705
OR
A330-300
POST 50088
OR
A330-800
POST 45556
OR
A330-800
POST 46554
OR
A330-800
POST 46582
OR
A330-800
POST 49705
OR
A330-800
POST 50088
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-38
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
383242-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
A330-900
POST 45556
OR
A330-900
POST 46554
OR
A330-900
POST 46582
OR
A330-900
POST 49705
OR
A330-900
POST 50088
384142-01-1
152 AIR SUPPLY SYSTEM
CA
DIS
I:
4 C
MRB 6,9
DISCARD SYSTEM FILTER ELEMENT.
384100-920-801
MRB REFERENCE:
38.40.00/02
ACCESS: 152JW
384200-01-1
172 AIR SUPPLY SYSTEM
*
CA
DET
I: 24000 FH
MRB 9
DETAILED INSPECTION OF COMPRESSOR INLET FILTER.
384200-200-801
1
MRB REFERENCE:
38.40.00/01
ACCESS: 162ZW
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
1
*
REV. DATE: JUL 01/21
SECTION:
2-38
0.40 A330-200
OR
A330-300
OR
0.20 A330-800
OR
A330-900
0.10 A330-200
POST 40243
(38-3029)
OR
0.02 A330-300
POST 40243
(38-3029)
OR
A330-800
POST 40243
(38-3029)
OR
A330-900
POST 40243
(38-3029)
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
384242-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
172 AIR SUPPLY SYSTEM
CA
DIS
I:
4 C
SOURCE
MRB 9
DISCARD COMPRESSOR OUTLET FILTER ELEMENT.
E N D
SYSTEMS, APU AND POWER PLANT : WATER/WASTE
384200-920-801
MRB REFERENCE:
38.40.00/03
ACCESS: 162ZW
* * * * *
REFERENCE
MEN
1
*
M/H
APPLICABILITY
0.40 A330-200
POST 40243
(38-3029)
OR
0.02 A330-300
POST 40243
(38-3029)
OR
A330-800
POST 40243
(38-3029)
OR
A330-900
POST 40243
(38-3029)
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -38
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
464000-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CABIN INFORMATION NETWORK
AV
RST
I:
24 MO
SOURCE
MRB 7
CALIBRATION OF BASE TRANSCEIVER STATION.
464100-01-1
120 CABIN INFORMATION NETWORK
AF
DIS
I:
2400 FH
MRB 9
464100-920-801
210 ON-BOARD INFORMATION TERMINAL (OIT)
AF
OPC
I: 10000 FH
CMR*
210 ON-BOARD INFORMATION TERMINAL (OIT)
AF
OPERATIONAL CHECK OF OIT CONNECTION TO AIRCRAFT
BATTERY.
465500-710-807
I:
6000 FH
CMP
CMR*
465500-710-807
CMP REFERENCE:
46-2-0000-001
CMR REFERENCE:
465500-00001-1-C
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : INFORMATION SYSTEMS
APPLICABILITY
0.15 A330-200
IF ALNA V2.1 WITH
OMTS INSTALLED AND
ACTIVATED
OR
A330-300
IF ALNA V2.1 WITH
OMTS INSTALLED AND
ACTIVATED
1
0.15 ALNA-RACK WITH
AIR-FILTERS
INSTALLED
1
0.10 POST 58865
(46-3059)
PRE 202854
(46-3102)
NON-ETOPS
OR
POST 58865
(46-3059)
PRE 202854
(46-3102)
ETOPS
UP TO 180 MIN D.T.
OR
POST 201482
NON-ETOPS
OR
POST 201482
ETOPS
UP TO 180 MIN D.T.
1
0.10 POST 58865
(46-3059)
ETOPS
BEYOND 180 MIN D.T.
OR
POST 201482
ETOPS
CMR REFERENCE:
465500-00001-1-C
OPC
M/H
1
MRB REFERENCE:
46.40.00/02
OPERATIONAL CHECK OF OIT CONNECTION TO AIRCRAFT
BATTERY.
465500-01-2
443400-820-801
MEN
MRB REFERENCE:
46.40.00/01
DISCARD ALNA RACK FILTER ELEMENTS.
465500-01-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-46
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
465500-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
BEYOND 180 MIN D.T.
465500-02-1
210 ON-BOARD INFORMATION TERMINAL (OIT)
AF
OPC
I:
8000 FH
CMR*
OPERATIONAL CHECK OF OIT SHEDDING IN LAND RECOVERY
CONFIGURATION.
* * * * *
E N D
465500-710-808
CMR REFERENCE:
465500-00002-1-C
1
0.15 POST 202475
PRE 205331
(46-3120)
* * * * *
SYSTEMS, APU AND POWER PLANT : INFORMATION SYSTEMS
REV. DATE: JUL 01/21
SECTION:
2 -46
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
470000-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
191 INERT GAS SYSTEM
AF
DIS
I:
7000 FH
SOURCE
MRB 9
DISCARD FILTER ELEMENT.
191 INERT GAS SYSTEM
AF
DIS
I: 27000 FH
MRB 7
DISCARD AIR SEPARATOR MODULES.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : FUEL TANK INERTING
471041-920-801
MRB REFERENCE:
47.00.00/01
ACCESS: 191LB
470000-02-1
REFERENCE
471043-920-801
MRB REFERENCE:
47.00.00/02
MEN
1
*
2
M/H
APPLICABILITY
0.20 A330-200
POST 58020
(47-3002),
(47-3005),
0.15 (47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
OR
A330-200F
POST 58020
(47-3002),
(47-3005),
(47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
PRE 58623
OR
A330-200F
POST 58020
(47-3002),
(47-3005),
(47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
POST 200281
OR
A330-300
POST 58020
POST 58166
OR
A330-800
OR
A330-900
3.50 A330-200
POST 58020
(47-3002),
(47-3005),
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -47
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
470000-02-1
ZONE
* * * * *
ACCESS: 191KB
470000-05-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
REFERENCE
191LB
AF
OPC
I: 12000 FH
FAL
OPERATIONAL CHECK OF DUAL FLAPPER CHECK VALVES (DFCV)
FOR REVERSE FLOW.
472043-710-804
APPLICABILITY
*
2.15 (47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
OR
A330-200F
POST 58020
(47-3002),
(47-3005),
(47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
PRE 58623
OR
A330-200F
POST 58020
(47-3002),
(47-3005),
(47-3008)
POST 58166
(47-3002),
(47-3005),
(47-3008)
POST 200281
OR
A330-300
POST 58020
POST 58166
OR
A330-800
OR
A330-900
1
0.80 A330-200
POST 58019
(47-3001)
PRE 58020
(47-3002),
1.70 (47-3005)
FAL REFERENCE:
470000-00003-1-F
ACCESS: 191FB
*
E N D
M/H
* * * * *
191 INERT GAS SYSTEM
* * * * *
MEN
* * * * *
SYSTEMS, APU AND POWER PLANT : FUEL TANK INERTING
REV. DATE: JUL 01/21
SECTION:
2 -47
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
491200-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
315 APU MOUNTS
AF
DET
I: 12000 FH
SOURCE
MRB 9
DETAILED INSPECTION OF APU SUSPENSION SYSTEM RODS AND
ATTACHMENT FITTINGS FOR CONDITION AND SECURITY.
ACCESS: 315AL
491200-02-1
REFERENCE
491200-200-801
DET
M/H
APPLICABILITY
1
0.50 ALL
*
0.08
1
1
0.25 ALL
0.25
*
*
0.04
0.04
1
0.20 ALL
*
0.08
1
0.13 ALL
1
0.10 NON-ETOPS
MRB REFERENCE:
49.12.00/01-35
316AR
315 APU MOUNTS
AF
316
DETAILED INSPECTION OF VIBRATION ISOLATORS AND
BRACKETS FOR CONDITION AND SECURITY.
MEN
I: 12000 FH
MRB 9
491200-200-806
MRB REFERENCE:
49.12.00/02-35
NOTE:
ETOPS RELEVANT
ACCESS: 315AL
316AR
491300-01-1
310 FIRE SEALS
AF
GVI
I: 12000 FH
MRB 8
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE
SEALS, WALLS INCLUDING FORWARD, AFT, UPPER, SIDES AND
COMPARTMENT DOORS.
ACCESS: 315AL
491600-03-1
491300-200-801
MRB REFERENCE:
49.13.00/01-35
316AR
300 AIR INTAKE SYSTEM
EN
GVI
I: 20000 FH
MRB 9
GENERAL VISUAL INSPECTION OF DIVERTER.
491600-200-803
MRB REFERENCE:
49.16.00/03-35
NOTE:
ETOPS RELEVANT
493100-01-2
310 APU FUEL DISTRIBUTION
EN
VCK
VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR
BUTTON ON FUEL FILTER.
T:
150 FH
MRB 9
493241-210-801
I:
1500 AH
NOTE
MRB REFERENCE:
49.30.00/01-35
REV. DATE: JUL 01/21
SECTION:
NOTE:
- TASK TO BE ACCOMPLISHED AT 150FH, 400FH, AND 800FH
AFTER AIRCRAFT DELIVERY. THEREAFTER EVERY 1500 AH.
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AUXILARY POWER UNIT
* * * * *
2-49
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
493100-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.08
1
0.10 ETOPS
*
0.08
1
0.33 ALL
*
0.01
1
0.33 ALL
* * * * *
- TASK TO BE ACCOMPLISHED AT 150FH AND 400FH AFTER
MAJOR TANK REPAIR. THEREAFTER EVERY 1500 AH.
- ETOPS RELEVANT
ACCESS: 315AL
R
493100-01-3
316AR
310 APU FUEL DISTRIBUTION
EN
VCK
VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR
BUTTON ON FUEL FILTER.
T:
150 FH
I:
1500 AH
NOTE
CMP
MRB 9
NOTE:
- TASK TO BE ACCOMPLISHED AT 150FH, 400FH, AND 800FH
AFTER AIRCRAFT DELIVERY. THEREAFTER EVERY 1500 AH.
- TASK TO BE ACCOMPLISHED AT 150FH AND 400FH AFTER
MAJOR TANK REPAIR. THEREAFTER EVERY 1500AH.
- ETOPS RELEVANT
ACCESS: 315AL
496200-01-1
493241-210-801
CMP REFERENCE:
49-2-2003-002
MRB REFERENCE:
49.30.00/01-35
316AR
210 EMERGENCY SHUTDOWN
EN
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING
APU STOP SWITCH 1KL.
496200-710-801
MRB REFERENCE:
49.62.00/01-35
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
496200-02-1
ACCESS: 121EL
496200-02-1
210 EMERGENCY SHUTDOWN
EN
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING
APU STOP SWITCH 2KL.
496200-710-803
MRB REFERENCE:
49.62.00/02-35
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
496200-01-1
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : AUXILARY POWER UNIT
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-49
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
496200-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
310 APU EXHAUST
EN
DET
I: 24000 FH
MRB 9
DETAILED INSPECTION OF SEALING RING COUPLING AND
BELLOWS.
ACCESS: 315AL
498100-02-1
EN
499100-01-2
316AR
DET
I: 12000 FH
MRB 9
EN
VCK
I:
500 AH
CMP
MRB 9
0.01
1
0.50 ALL
*
0.08
1
0.33 ALL
*
0.11
499141-210-801
1
0.10 PRE 56284
(49-3028)
APU WITH OIL PUMP
PN 3881000-6
INSTALLED
*
0.08
CMP REFERENCE:
49-2-2003-003
MRB REFERENCE:
49.90.00/01-35
49.90.00/02-35
316AR
E N D
*
MRB REFERENCE:
49.80.00/01-35
CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON
- ON LUBE FILTER
- ON GENERATOR SCAVENGE FILTER.
* * * * *
498145-210-801
317AL
310 APU OIL SYSTEM
ACCESS: 315AL
APPLICABILITY
MRB REFERENCE:
49.80.00/03-35
DETAILED INSPECTION OF V-CLAMP, EXHAUST DUCT AND
EXHAUST DUCT HEAT INSULATION.
R
498145-210-802
316AR
310 APU EXHAUST
ACCESS: 315AL
M/H
* * * * *
ACCESS: 198DB
498100-01-1
MEN
* * * * *
SYSTEMS, APU AND POWER PLANT : AUXILARY POWER UNIT
REV. DATE: JUL 01/21
SECTION:
2-49
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
521000-01-1
521000-02-1
521000-03-1
ZONE
831
832
833
841
842
843
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
PASSENGER/CREW DOORS
AF
FNC
I:
48 MO
SOURCE
MRB 6,9
FUNCTIONAL CHECK OF LOCKING MECHANISM.
831 PASSENGER/CREW DOORS
AF
OPC
832
833 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR
841 IS OPENED FROM OUTSIDE.
842
843
I:
831
832
833
841
842
843
I:
AF
OPC
521000-720-801
MRB REFERENCE:
52.10.00/04
NOTE:
TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY
DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY
USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT
EMERGENCY EXIT. REFER TO MPD 522200-02-1.
PASSENGER/CREW DOORS
REFERENCE
48 MO
MRB 9
521000-710-804
MRB REFERENCE:
52.10.00/05
24 MO
MRB 9
OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN
POSITION.
521000-710-802
MRB REFERENCE:
52.10.00/02
NOTE:
TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY
DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY
USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT
EMERGENCY EXIT. REFER TO MPD 522200-01-1.
ACCESS: 831
832
833
841
842
843
SYSTEMS, APU AND POWER PLANT : DOORS
MEN
M/H
1
1
1
1
1
1
0.05
0.05
0.05
0.05
0.05
0.05
SECTION:
2-52
A330-200
DOORS USED
REGULARLY,
OR
A330-300
DOORS USED
REGULARLY,
OR
A330-800
DOORS USED
REGULARLY,
OR
A330-900
DOORS USED
REGULARLY,
2
2
2
2
2
2
0.30 ALL
0.30
0.30
0.30
0.30
0.30
1
1
1
1
1
1
0.05
0.05
0.05
0.05
0.05
0.05
*
*
*
*
*
*
REV. DATE: JUL 01/21
APPLICABILITY
0.02
0.02
0.02
0.02
0.02
0.02
A330-200
DOORS USED
REGULARLY,
OR
A330-300
DOORS USED
REGULARLY,
OR
A330-800
DOORS USED
REGULARLY,
OR
A330-900
DOORS USED
REGULARLY,
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
521000-04-1
R
N
521000-07-1
521000-07-2
521000-10-1
ZONE
831
832
833
841
842
843
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
PASSENGER/CREW DOORS
AF
OPC
I:
72 MO
SOURCE
MRB 9
OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING
LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS
OPEN.
I:
831
832
833
841
842
843
T:
24 MO
NOTE
I:
24 MO
NOTE
AF
FNC
FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR
SLIDER MECHANISM.
521000-710-805
MRB REFERENCE:
52.10.00/06
831 PASSENGER/CREW DOOR
AF
FNC
832
833 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR
841 SLIDER MECHANISM.
842
843
PASSENGER/CREW DOOR
REFERENCE
24 MO
MRB 8
521000-200-805
MRB REFERENCE:
52.10.00/09
MRB 8
SEMR
521000-200-805
MRB REFERENCE:
52.10.00/09
NOTE:
- NO SHORT-TERM EXTENSION IS ALLOWED
SEMR REFERENCE:
521000-00001-1-E
831 PASSENGER/CREW DOORS
AF
LUB
841
LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL
HANDLE.
I:
24 MO
MRB 6,9
122252-600-812
831 PASSENGER/CREW DOORS
AF
841
OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN
POSITION.
OPC
I:
24 MO
MRB 9
521000-710-806
MRB REFERENCE:
52.10.00/11
ACCESS: 831
841
SYSTEMS, APU AND POWER PLANT : DOORS
M/H
APPLICABILITY
1
1
1
1
1
1
0.30 ALL
0.30
0.30
0.30
0.30
0.30
1
1
1
1
1
1
0.30
0.30
0.30
0.30
0.30
0.30
1
1
1
1
1
1
0.30 A330-800
0.30
0.30
0.30
0.30
0.30
1
1
0.10 A330-200F
0.10
*
*
0.02
0.02
1
1
0.05 A330-200F
0.05
*
*
0.02
0.02
A330-200
OR
A330-200F
OR
A330-300
OR
A330-900
MRB REFERENCE:
52.10.00/10
ACCESS: 831
841
521000-11-1
MEN
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
521000-12-1
N
521000-13-1
521121-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
831 PASSENGER/CREW DOORS
841
FUNCTIONAL CHECK OF LOCKING MECHANISM.
AF
FNC
I:
MRB 6,9
REFERENCE
521000-720-802
I:
831
832
833
841
842
843
I:
AF
LUB
1000 FH
MRB 9
521000-210-801
MRB REFERENCE:
52.10.00/13
24 MO
MRB 6,9
LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL
HANDLE.
122252-600-802
MRB REFERENCE:
52.10.00/01
NOTE:
TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY
DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY
USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT
EMERGENCY EXIT. REFER TO MPD 522200-03-1.
ACCESS: 831
832
833
841
842
843
R
522200-01-1
522200-02-1
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
844
OPERATIONAL CHECK OF DOOR UNLOCKING/LOCKING AND DOOR
OPENING/CLOSING FROM INSIDE AND OUTSIDE AND DOOR
LATCHING IN FULLY OPEN POSITION, AND ACTUATOR
DAMPENING AND FRICTIONLESS EXTENSION/RETRACTION.
I:
832 PASSENGER COMPARTMENT EMERGENCY EXIT
833
834 FUNCTIONAL CHECK OF LOCKING MECHANISM.
I:
* * * * *
SYSTEMS, APU AND POWER PLANT : DOORS
C O N T I N U E D
MEN
1
1
M/H
APPLICABILITY
0.05 A330-200F
0.05
MRB REFERENCE:
52.10.00/12
831 PASSENGER/CREW DOORS
AF
FNC
832
833 CHECK OF EMERGENCY ACCUMULATOR CYLINDER PRESSURE.
841
842
843
PASSENGER/CREW DOORS
48 MO
SOURCE
AF
FNC
24 MO
MRB 8
522200-710-801
1
1
1
1
1
1
1
1
1
1
1
1
MRB 8
522200-720-801
MRB REFERENCE:
0.10
0.10
0.10
0.10
0.10
0.10
A330-200
DOORS USED
REGULARLY,
OR
A330-300
DOORS USED
REGULARLY,
OR
A330-800
DOORS USED
REGULARLY,
OR
A330-900
DOORS USED
REGULARLY,
*
*
*
*
*
*
0.02
0.02
0.02
0.02
0.02
0.02
2
2
0.20 A330-200
0.20 OR
A330-300
OR
A330-800
OR
A330-900
1
1
1
0.10 A330-200
0.10 OR
0.10 A330-300
MRB REFERENCE:
52.22.00/03
48 MO
TBD ALL
TBD
TBD
TBD
TBD
TBD
SEE NOTE
SEE NOTE
SEE NOTE
SEE NOTE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
522200-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
522200-04-1
522200-05-1
522200-06-1
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
LUB
844
LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL
HANDLE.
I:
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
844
OPERATIONAL CHECK OF DOOR DAMPING, ESCAPE SLIDE
RELEASE MECHANISM DISARMING, AND TO ENSURE THAT DOOR
CANNOT BE LOWERED AND LOCKED WHEN OPEN.
I:
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
844
OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR
IS OPENED FROM OUTSIDE.
I:
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
844
OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING
LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS
OPEN.
I:
SYSTEMS, APU AND POWER PLANT : DOORS
MEN
M/H
APPLICABILITY
* * * * *
842
843
844
522200-03-1
REFERENCE
24 MO
MRB 8
52.22.00/05
1
1
1
0.10 OR
0.10 A330-800
0.10 OR
A330-900
122252-600-807
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
2
2
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
A330-900
1
1
0.10 A330-200
0.10 OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
52.22.00/02
24 MO
MRB 9
522200-710-802
MRB REFERENCE:
52.22.00/01
48 MO
MRB 9
522200-710-803
MRB REFERENCE:
52.22.00/04
72 MO
MRB 9
522200-710-804
MRB REFERENCE:
52.22.00/06
REV. DATE: JUL 01/21
SECTION:
2-52
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
N
522200-09-1
522200-09-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
FNC
844
FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR
SLIDER MECHANISM.
I:
24 MO
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
FNC
844
FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR
SLIDER MECHANISM.
T:
24 MO
NOTE
I:
24 MO
NOTE
SOURCE
MRB 8
821 FWD CARGO COMPARTMENT DOOR
MRB 8
SEMR
523100-02-1
132BR
132HR
821CR
132CR
132JR
821DR
132ER
132LR
821 FWD CARGO COMPARTMENT DOOR
LUB
I:
24 MO
MRB 6,9
523200-01-1
821BR
821CR
FNC
I:
72 MO
MRB 6,9
SYSTEMS, APU AND POWER PLANT : DOORS
152BR
152HR
822CR
152CR
152JR
822DR
523100-720-801
821DR
AF
152DR
152KR
152ER
152LR
0.30 A330-200
0.30 OR
A330-300
OR
A330-900
1
1
0.30 A330-800
0.30
1
0.50 ALL
*
1.06
1
1.20 ALL
*
0.75
1
0.50 ALL
*
1.07
MRB REFERENCE:
52.31.00/02
LUB
I:
24 MO
MRB 6,9
LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING -,
LATCHING - AND INTERLOCK MECHANISM.
ACCESS: 152AR
152GR
822BR
122252-600-801
132FR
821AR
AF
822 AFT CARGO COMPARTMENT DOOR
1
1
MRB REFERENCE:
52.31.00/01
FUNCTIONAL CHECK OF LATCHING AND LOCKING HANDLE
FORCES, AND OF WEAR AND OVERCENTER POSITIONS OF
LATCHING, LOCKING AND INTERLOCK MECHANISMS.
ACCESS: 821AR
APPLICABILITY
SEMR REFERENCE:
522200-00001-1-E
AF
132DR
132KR
522200-200-805
M/H
MRB REFERENCE:
52.22.00/09
LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING,
LATCHING AND INTERLOCK MECHANISMS.
ACCESS: 132AR
132GR
821BR
522200-200-805
MEN
MRB REFERENCE:
52.22.00/09
NOTE:
- NO SHORT-TERM EXTENSION IS ALLOWED.
523100-01-1
REFERENCE
122252-600-808
MRB REFERENCE:
52.31.00/01
152FR
822AR
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523200-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
822 AFT CARGO COMPARTMENT DOOR
AF
FNC
I:
72 MO
SOURCE
MRB 6,9
*
0.75
1
0.10 ALL
*
0.05
1
0.15 ALL
PREP.: DOOR LINING Z823;
*
0.20
ACCESS: 823
*
0.05
1
0.20 A330-200F
1
1.00 A330-200F
*
0.70
1
0.10 A330-200F
*
0.70
822BR
822CR
822DR
823 BULK CARGO COMPARTMENT DOOR
AF
OPC
I:
24 MO
MRB 9
523311-710-801
MRB REFERENCE:
52.33.00/01
ACCESS: 823
823 BULK CARGO COMPARTMENT DOOR
AF
LUB
I:
24 MO
MRB 6
LUBRICATION OF BULK CARGO COMPARTMENT DOOR
COMPONENTS.
523800-01-1
835 MAIN DECK CARGO COMPARTMENT DOOR
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
LUB
I:
24 MO
MRB 9
AF
FNC
I:
72 MO
MRB 6,9
AF
VCK
523800-720-801
MRB REFERENCE:
52.38.00/02
PREP.: LINING Z835;
835 MAIN DECK CARGO COMPARTMENT DOOR
122252-600-813
MRB REFERENCE:
52.38.00/01
FUNCTIONAL CHECK OF LATCHING AND LOCKING MECHANISM.
523800-03-1
122252-600-803
MRB REFERENCE:
52.33.00/03
LUBRICATION OF DOOR HINGE.
523800-02-1
APPLICABILITY
MRB REFERENCE:
52.31.00/02
OPERATIONAL CHECK OF DOOR BALANCE MECHANISM AND OF
DOOR LATCHING IN FULLY OPEN POSITION.
523300-03-1
M/H
1.20 ALL
ACCESS: 822AR
523200-720-801
MEN
1
FUNCTIONAL CHECK OF LATCHING AND LOCKING HANDLE
FORCES, AND OF WEAR AND OVERCENTER POSITIONS OF
LATCHING, LOCKING AND INTERLOCK MECHANISMS.
523300-01-1
REFERENCE
I:
72 MO
MRB 9
VISUAL CHECK OF DRAIN VALVES.
523811-200-801
MRB REFERENCE:
52.38.00/03
PREP.: LINING Z835;
SYSTEMS, APU AND POWER PLANT : DOORS
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523800-07-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
LUB
I:
18 MO
SOURCE
MRB 6,9
LUBRICATION OF LATCHING MECHANISM, LOCKING MECHANISM,
SEQUENCE SHAFT AND INTERLOCK MECHANISM.
REFERENCE
122252-600-811
525111-01-1
835BL
835CL
210 COCKPIT DOOR
AF
FNC
I:
42 MO
MRB 9
FUNCTIONAL CHECK OF SPRING LOADED DOOR STOP
MECHANISM.
525111-02-1
220 COCKPIT DOOR
DET
I:
48 MO
MRB 6,9
DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR
LOCKING SYSTEM.
SYSTEMS, APU AND POWER PLANT : DOORS
APPLICABILITY
1
1.00 A330-200F
*
0.70
*
0.43
525111-720-801
1
0.20 A330-200
PRE 50014
(25-3161),
(25-3194)
OR
A330-300
PRE 50014
(25-3161),
(25-3194)
1
0.50 A330-200
POST 50014
(25-3161),
(25-3194)
OR
A330-200F
POST 58673
(25-3625)
OR
A330-300
POST 50014
(25-3161),
(25-3194)
OR
A330-800
POST 50014
(25-3161),
(25-3194)
OR
A330-900
POST 50014
(25-3161),
(25-3194)
MRB REFERENCE:
52.51.11/01
AF
M/H
MRB REFERENCE:
52.38.00/07
PREP.: LINING Z835;
ACCESS: 835AL
MEN
525100-200-801
MRB REFERENCE:
52.51.11/02
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
525111-03-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
220 COCKPIT DOOR
AF
OPC
I:
48 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS
FOR RAPID DECOMPRESSION, CHECK OF DOOR OPENING IN
CASE OF POWER OFF AND BY USING THE EMERGENCY CODE.
525111-04-1
220 COCKPIT DOOR
AF
REFERENCE
525100-710-805
MEN
I:
OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE
MECHANISM.
48 MO
OR
12000 FH
CMR**
MRB 8
256800-710-804
1.00 A330-200
POST 50014
(25-3161),
(25-3194)
OR
A330-200F
POST 58673
(25-3625)
OR
A330-300
POST 50014
(25-3161),
(25-3194)
OR
A330-800
POST 50014
(25-3161),
(25-3194)
OR
A330-900
POST 50014
(25-3161),
(25-3194)
1
0.10 A330-200
POST 50014
(25-3161),
(25-3194)
PRE 57371
(25-3493)
OR
A330-300
POST 50014
(25-3161),
(25-3194)
PRE 57371
(25-3493)
1
0.20 A330-200
POST 50014
(25-3161),
(25-3194)
PRE 57371
CMR REFERENCE:
525111-00001-1-C
MRB REFERENCE:
52.51.11/04
525111-05-1
220 COCKPIT DOOR
AF
DET
I:
48 MO
MRB 8
DETAILED INSPECTION OF FLAP BELLOW.
* * * * *
SYSTEMS, APU AND POWER PLANT : DOORS
C O N T I N U E D
256800-220-801
MRB REFERENCE:
52.51.11/05
APPLICABILITY
1
MRB REFERENCE:
52.51.11/03
OPC
M/H
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
525111-05-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
(25-3493)
OR
A330-300
POST 50014
(25-3161),
(25-3194)
PRE 57371
(25-3493)
R
525111-06-1
220 COCKPIT DOOR
AF
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF MANUAL SWITCH OVERRIDE.
525111-07-1
220 COCKPIT DOOR
AF
220 COCKPIT DOOR
OPC
I:
72 MO
MRB 8
AF
SYSTEMS, APU AND POWER PLANT : DOORS
C O N T I N U E D
0.10 POST 50723
(52-3067)
OR
POST 53123
GVI
256800-710-805
1
0.10 A330-200
POST 57371
(25-3493)
OR
A330-200F
POST 58673
(25-3625)
OR
A330-300
POST 57371
(25-3493)
OR
A330-800
POST 57371
(25-3493)
OR
A330-900
POST 57371
(25-3493)
1
0.10 A330-200
POST 57371
(25-3493)
OR
A330-200F
POST 58673
MRB REFERENCE:
52.51.11/07
I:
72 MO
MRB 8
GENERAL VISUAL INSPECTION OF AIR CYLINDER OF
DECOMPRESSION PANEL.
* * * * *
2
MRB REFERENCE:
52.51.11/06
OPERATIONAL CHECK OF FLAP RELEASE MECHANISM (MANUAL
OPENING).
525111-08-1
525100-710-806
256800-210-803
MRB REFERENCE:
52.51.11/08
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
525111-08-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
(25-3625)
OR
A330-300
POST 57371
(25-3493)
OR
A330-800
POST 57371
(25-3493)
OR
A330-900
POST 57371
(25-3493)
527100-01-1
210 DOOR WARNING SYSTEM
AF
OPC
I:
72 MO
MRB 9
OPERATIONAL CHECK OF DOOR WARNING SYSTEM.
527100-02-1
210 DOOR AND ESCAPE SLIDE RELEASE CONTROL
R
527100-04-1
1
0.50 ALL
1
0.50 ALL
1
1
1
0.40 ALL
0.40
0.40
1
0.40 ALL
MRB REFERENCE:
52.70.00/01
AF
OPC
I:
48 MO
MRB 9
OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE
WARNING SYSTEM.
527100-03-1
527100-710-801
MRB REFERENCE:
52.70.00/04
100 DOOR AND ESCAPE SLIDE CONTROL
AF
FNC
120
200 OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING
SYSTEM AND FUNCTIONAL CHECK OF ASSOCIATED PRESSURE
SWITCH.
I:
210 DOOR AND ESCAPE SLIDE CONTROL
I:
AF
FNC
527100-710-802
72 MO
MRB 9
527100-710-803
MRB REFERENCE:
52.70.00/05
8 MO
MRB 9
CHECK BATTERY CAPACITY OF AUTONOMOUS STANDBY POWER
SUPPLY UNIT (ASPSU).
527100-740-803
MRB REFERENCE:
52.70.00/02
NOTE:
AS AN ALTERNATIVE, TASK MAY BY ACCOMPLISHED BY
REPLACING BATTERIES BY FULLY-CHARGED UNITS (REF. AMM
527136/4, 52-71-36-000-802) AND SENDING REMOVED
* * * * *
SYSTEMS, APU AND POWER PLANT : DOORS
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-52
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
527100-04-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
BATTERIES TO WORKSHOP.
527100-07-1
210 DOOR AND ESCAPE SLIDE CONTROL
AF
OPC
I:
6000 FH
MRB 9
BITE TEST OF AUTONOMOUS STANDBY POWER SUPPLY UNIT
(ASPSU).
* * * * *
SYSTEMS, APU AND POWER PLANT : DOORS
E N D
527100-740-804
1
0.10 ALL
MRB REFERENCE:
52.70.00/03
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -52
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531900-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
100 FUSELAGE DRAINS
AF
OPC
I:
24 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF DRAIN HOLES IN LOWER PART OF FR
1 AND FR 80 (FROM INSIDE).
ACCESS: 121AF
531900-02-1
162ZW
811
530000-200-801
823
100 FUSELAGE DRAINS
AF
OPC
220 FUSELAGE DRAINS
AF
GVI
I:
24 MO
MRB 9
530000-200-802
I:
72 MO
MRB 9
531100-210-816
1
0.30 ALL
*
0.32
1
0.20 ALL
1
0.10 A330-200F
*
EL
APPLICABILITY
MRB REFERENCE:
53.19.00/10
PREP.: BARRIER WALL INSULATION;
BARRIER WALL LINING;
120 FUSELAGE DRAINS
M/H
MRB REFERENCE:
53.19.00/05
GENERAL VISUAL INSPECTION OF DRAIN FUNNEL(S) IN
BARRIER WALL.
531900-11-1
MEN
MRB REFERENCE:
53.19.00/01
OPERATIONAL CHECK OF DRAIN HOLES IN UNPRESSURIZED
PART OF FUSELAGE (IN RADOME, FORWARD OF FR 1, BEHIND
REAR PRESSURE BULKHEAD, IN BELLY FAIRING, TAIL CONE
AND IN CARGO COMPARTMENT DOORS).
531900-03-1
REFERENCE
OPC
I:
OPERATIONAL CHECK OF DRAIN TUBES OF THE ELECTRONICS
RACK 800VU.
24 MO
NOTE
MRB 9
257142-200-801
TBD
1
0.10 A330-200F
*
0.11
1
1
1
0.15 ALL
0.15
0.15
MRB REFERENCE:
53.19.00/11
NOTE:
INTERVAL:
- OPERATORS ARE ADVISED TO OPTIMISE THE INTERVAL OF
THIS TASK ACCORDING TO THEIR OPERATING ENVIRONMENT
AND EXPERIENCE. THIS MAY RESULT IN A LESS OR MORE
FREQUENT INTERVAL
ACCESS: 132AZ
532900-01-1
821
100 FUSELAGE DRAINS
AF
OPC
821
822 OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES IN
LOWER FUSELAGE SHELL (FROM OUTSIDE) AND IN FWD AND
AFT CARGO COMPARTMENT DOORS.
SYSTEMS, APU AND POWER PLANT : FUSELAGE
I:
24 MO
MRB 9
530000-200-803
MRB REFERENCE:
53.19.00/02
REV. DATE: JUL 01/21
SECTION:
2 -53
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532900-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
100 FUSELAGE DRAINS
AF
GVI
I:
72 MO
SOURCE
MRB 9
GENERAL VISUAL INSPECTION OF HOLES OF PISTON TYPE
DRAIN OR PRESSURE DRAIN VALVES AND PRESSURE SEAL
DRAINS FROM INSIDE (IN FUSELAGE BILGE AREA, AT UPPER
AFT END OF CENTER WING BOX AND IN CARGO COMPARTMENT
DOORS).
REFERENCE
530000-200-804
140 FUSELAGE DRAINS
*
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT UPPER
AFT END OF CENTER WING BOX (FROM MAIN LANDING GEAR
BAY).
ACCESS: 734
534900-01-1
AF
OPC
310 REAR FUSELAGE DRAIN
AF
I:
24 MO
MRB 9
SYSTEMS, APU AND POWER PLANT : FUSELAGE
E N D
0.50 ALL
>99.9
1
0.10 ALL
*
0.30
530000-200-805
1
0.10 ALL
1
0.05 ALL
MRB REFERENCE:
53.19.00/09
OPC
I:
6 MO
MRB 9
OPERATIONAL CHECK OF DRAIN MAST/PIPES AFT OF FR 80.
* * * * *
APPLICABILITY
MRB REFERENCE:
53.19.00/03
OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT BULK
CARGO COMPARTMENT DOOR (FROM OUTSIDE).
535900-01-1
533900-200-801
744
823 FUSELAGE DRAINS
1
M/H
MRB REFERENCE:
53.19.00/06
PREP.: FLOOR PANELS Z120;
FLOOR PANELS Z130;
FLOOR PANELS Z150;
FLOOR PANELS Z160;
FLOOR PANELS Z250;
INSULATION Z821;
INSULATION Z822;
LD-MCR IF INSTALLED;
LINING Z821;
LINING Z822;
533900-01-1
MEN
530000-200-806
MRB REFERENCE:
53.19.00/04
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -53
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
545100-02-1
ZONE
450 NACELLE/PYLON DRAIN (GE CF6-80E1)
AF
OPC
460
OPERATIONAL CHECK OF COMPARTMENT A, C AND F AND OF
HYDRAULIC AND FUEL PAN DRAIN SYSTEM.
ACCESS: 415AL
453BL
425AL
463BL
545100-03-1
417AL
453CR
427AL
463CR
418AR
454CL
428AR
464CL
416AR
453CL
426AR
463CL
417AL
453CR
427AL
463CR
418AR
454CL
428AR
464CL
416AR
453CL
426AR
463CL
417AL
453CR
427AL
463CR
418AR
454CL
428AR
464CL
I:
48 MO
SOURCE
MRB 8
REFERENCE
545000-200-812
MEN
M/H
1
1
0.30 GE
0.30
APPLICABILITY
MRB REFERENCE:
54.59.00/01-G6
451DL
452CL
*
1.10
461DL
462CL
*
1.10
1
1
0.30 PW
0.30
I:
48 MO
MRB 8
545000-200-813
MRB REFERENCE:
54.59.00/01-PW
451DR
452CL
*
1.10
461DR
462CL
*
1.10
1
1
0.30 TRENT 700
0.30
450 PYLON DRAINS (RR TRENT768/772)
AF
OPC
460
OPERATIONAL CHECK OF COMPARTMENT A, C AND F DRAIN
SYSTEM.
ACCESS: 415AL
453BL
425AL
463BL
545100-05-1
416AR
453CL
426AR
463CL
450 NACELLE/PYLON DRAIN (PW 4000)
AF
OPC
460
OPERATIONAL CHECK OF COMPARTMENT A, C AND F AND OF
HYDRAULIC AND FUEL PAN DRAIN SYSTEM.
ACCESS: 415AL
453BL
425AL
463BL
545100-04-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
I:
48 MO
MRB 8
545000-200-814
MRB REFERENCE:
54.59.00/01-RR
451DR
452CL
*
1.10
461DR
462CL
*
1.10
1
1
0.20 GE
0.20
*
*
0.95
0.95
450 NACELLE/PYLON DRAIN (GE CF6-80E1)
AF
DET
460
DETAILED INSPECTION OF COMPARTMENT A AND F DRAIN LINE
INSTALLED UNDERNEATH LAPF INTERFACE WITH LAPF
REMOVED.
I:
42 MO
MRB 8
545000-220-805
MRB REFERENCE:
54.59.00/02-G6
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-08-1
ACCESS: 415AL
425AL
416AR
426AR
SYSTEMS, APU AND POWER PLANT : NACELLES/PYLONS
417AL
427AL
418AR
428AR
454AL
464AL
REV. DATE: JUL 01/21
SECTION:
2-54
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
545100-06-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
450 NACELLE/PYLON DRAIN (PW 4000)
AF
DET
460
DETAILED INSPECTION OF COMPARTMENT A AND F DRAIN LINE
WITH LAPF REMOVED.
I:
42 MO
SOURCE
MRB 8
REFERENCE
545000-220-807
MEN
M/H
APPLICABILITY
1
1
0.20 PW
0.20
*
*
0.88
0.88
1
1
0.20 TRENT 700
0.20
*
*
0.75
0.75
1
1
0.60 GE
0.60
1
1
0.60 PW
0.60
MRB REFERENCE:
54.59.00/02-PW
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-09-1
ACCESS: 415BL
425BL
545100-07-1
416BR
426BR
417AL
427AL
418AR
428AR
454AL
464AL
450 PYLON DRAINS (RR TRENT768/772)
AF
DET
460
DETAILED INSPECTION OF COMPARTMENT A AND F DRAIN LINE
INSTALLED UNDERNEATH LAPF INTERFACE WITH LAPF
REMOVED.
I:
42 MO
MRB 8
545000-220-806
MRB REFERENCE:
54.59.00/02-RR
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-10-1.
ACCESS: 454AL
464AL
545100-08-1
450 NACELLE/PYLON DRAIN (GE CF6-80E1)
NDT SDI
460
SPECIAL DETAILED (BOROSCOPE) INSPECTION OF
COMPARTMENT A AND F DRAIN LINE INSTALLED UNDERNEATH
LAPF INTERFACE WITH LAPF INSTALLED.
I:
42 MO
MRB 8
545000-290-805
MRB REFERENCE:
54.59.00/03-G6
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-05-1
545100-09-1
450 NACELLE/PYLON DRAIN (PW 4000)
NDT SDI
460
SPECIAL DETAILED (BOROSCOPE) INSPECTION OF
COMPARTMENT A AND F DRAIN LINE WITH LAPF INSTALLED.
I:
42 MO
MRB 8
545000-290-807
MRB REFERENCE:
54.59.00/03-PW
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-06-1
SYSTEMS, APU AND POWER PLANT : NACELLES/PYLONS
REV. DATE: JUL 01/21
SECTION:
2 -54
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
545100-10-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
450 NACELLE/PYLON DRAIN (RR TRENT 768/772)
NDT SDI
460
SPECIAL DETAILED (BOROSCOPE) INSPECTION OF
COMPARTMENT A AND F DRAIN LINE INSTALLED UNDERNEATH
LAPF INTERFACE WITH LAPF INSTALLED.
I:
42 MO
SOURCE
MRB 8
REFERENCE
545000-290-806
MEN
M/H
APPLICABILITY
1
1
0.60 TRENT 700
0.60
1
1
0.34 TRENT 7000
0.34
1
1
0.05 TRENT 7000
0.05
1
1
0.25 TRENT 7000
0.25
1
1
0.20 TRENT 7000
0.20
MRB REFERENCE:
54.59.00/03-RR
NOTE:
- THIS TASK IS AN ALTERNATIVE TASK TO 545100-07-1
545900-N6-1
545900-N8-1
545900-N9-1
545901-N1-1
450 PYLON DRAINS
EN
OPC
460
OPERATIONAL AND VISUAL CHECK OF ZONES A, C, F1, F2
AND DOUBLE SKIN FUEL DRAIN.
I:
72 MO
OR
36000 FH
MRB 8
450 PYLON DRAINS
EN
460
DETAILED INSPECTION OF ME FINGER SEAL (AS FAR AS
VISIBLE).
I: 12000 FH
MRB 8
DET
545000-200-820
MRB REFERENCE:
54.59.00/06-RN
545000-220-814
MRB REFERENCE:
54.59.00/16-RN
450 PYLON DRAINS
AF
GVI
460
GENERAL VISUAL INSPECTION OF KARMAN FIRE SEALS (AS
FAR AS VISIBLE).
I: 12000 FH
450 PYLON DRAINS
AF
460
GENERAL VISUAL INSPECTION OF FAN FIRE SEALS.
I: 12000 FH
GVI
MRB 8
545000-210-801
MRB REFERENCE:
54.59.00/09-RN
MRB 8
545000-210-802
MRB REFERENCE:
54.59.00/10-RN
PREP.: FAN COWL OPEN;
545901-N2-1
545901-N3-1
450 PYLON DRAINS
460
GENERAL VISUAL INSPECTION OF FPS SEAL.
*
AF
GVI
450 PYLON DRAINS
AF
GVI
460
GENERAL VISUAL INSPECTION OF 2D-NACELLE FIRE SEAL.
SYSTEMS, APU AND POWER PLANT : NACELLES/PYLONS
I:
144 MO
MRB 8
545000-210-805
MRB REFERENCE:
54.59.00/11-RN
I: 12000 FH
MRB 8
545000-210-803
MRB REFERENCE:
54.59.00/12-RN
REV. DATE: JUL 01/21
SECTION:
2 -54
TBD
1
1
0.10 TRENT 7000
0.10
1
1
0.16 TRENT 7000
0.16
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
545901-N4-1
545901-N5-1
ZONE
DESCRIPTION
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
450 PYLON DRAINS
AF
GVI
460
GENERAL VISUAL INSPECTION OF RMF BLOCK SEAL AND RMF
FINGER SEAL.
I: 12000 FH
450 PYLON DRAINS
EN
GVI
460
GENERAL VISUAL INSPECTION OF AFT FAIRING LIP SEAL (AS
FAR AS VISIBLE).
I: 12000 FH
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : NACELLES/PYLONS
SOURCE
MRB 8
REFERENCE
545000-210-804
MEN
M/H
APPLICABILITY
1
1
0.10 TRENT 7000
0.10
1
1
0.20 TRENT 7000
0.20
MRB REFERENCE:
54.59.00/13-RN
MRB 8
545000-210-806
MRB REFERENCE:
54.59.00/14-RN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -54
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
551600-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
310 THS ATTACH FITTINGS
AF
LUB
I:
LUBRICATION OF THS HINGE LINE BEARINGS.
24 MO
OR
10000 FH
SOURCE
MRB 9
310 THS ATTACH FITTINGS
AF
LUBRICATION OF UPPER AND LOWER FRAME ATTACHMENT
BEARINGS.
LUB
I:
24 MO
OR
10000 FH
122253-600-801
MRB REFERENCE:
55.16.00/01
ACCESS: 313AL
551600-02-1
REFERENCE
MRB 9
122253-600-802
E N D
SYSTEMS, APU AND POWER PLANT : STABILIZERS
M/H
1
0.20 ALL
*
0.02
1
0.20 ALL
*
0.02
APPLICABILITY
MRB REFERENCE:
55.16.00/02
ACCESS: 313AL
* * * * *
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -55
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
561000-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
210 COCKPIT WINDOWS
AF
DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROM
OUTSIDE.
* * * * *
SYSTEMS, APU AND POWER PLANT : WINDOWS
E N D
DET
I:
12 MO
OR
6000 FH
SOURCE
MRB 6,9
REFERENCE
561000-200-802
MEN
1
M/H
APPLICABILITY
TBD ALL
MRB REFERENCE:
56.11.00/01
56.12.00/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -56
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
572900-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
540 SLAT TRACK CANS DRAIN
AF
OPC
640
OPERATIONAL CHECK OF DRAIN HOSES AND DESIGNATED DRAIN
HOLES FOR CLOGGING.
I:
72 MO
SOURCE
MRB 9
REFERENCE
572900-210-801
575900-01-1
535 WING TIP DRAIN
AF
635
OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING.
OPC
500 WING TRAILING AND LEADING EDGES DRAIN
AF
600
OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING.
OPC
* * * * *
SYSTEMS, APU AND POWER PLANT : WINGS
E N D
M/H
1
1
0.30 ALL
0.30
*
0.10
1
1
0.30 ALL
0.30
1
1
1.00 ALL
1.00
APPLICABILITY
MRB REFERENCE:
57.29.00/01
PREP.: SLATS EXTENDED;
573900-01-1
MEN
I:
72 MO
MRB 9
573900-210-801
MRB REFERENCE:
57.39.00/01
I:
72 MO
MRB 9
575900-210-801
MRB REFERENCE:
57.59.00/01
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-57
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
711100-G1-1
711300-G6-1
ZONE
410 AIR INTAKE COWL
EN
DET
420
DETAILED INSPECTION OF AIR INTAKE COWL INNER BARREL
ASSEMBLY.
I:
410 FAN COWL
EN
GVI
420
GENERAL VISUAL INSPECTION OF FIRESHIELD, FIRE SEALS
AND HEAT BLANKETS
I:
ACCESS: 414AL
424AL
711300-G7-1
711300-N1-1
711300-P1-1
711300-P4-1
711300-R4-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
414AR
424AR
415AL
425AL
416AR
426AR
417AL
427AL
MRB 9
REFERENCE
711141-220-801
EN
410 FAN COWL
420
FUNCTIONAL CHECK OF FAN COWL LATCH TENSION.
AF
FNC
18 MO
MRB 8
711300-210-806
I:
I:
411 FAN COWLS
EN
DET
421
DETAILED INSPECTION OF AIR INTAKE COWL LIP AND INNER
SKIN.
I:
410 FAN COWL
420
FUNCTIONAL CHECK OF FAN COWL LATCH TENSION.
AF
I:
410 FAN COWL
420
FUNCTIONAL CHECK OF FAN COWL LATCH TENSION.
AF
FNC
M/H
APPLICABILITY
1
1
0.10 GE
0.10
1
1
0.30 GE
0.30
*
*
0.30
0.30
1
1
0.25 GE
0.25
1
1
0.07 TRENT 7000
0.07
1
1
0.40 PW
0.40
1
1
0.30 PW
0.30
1
1
0.25 TRENT 700
0.25
MRB REFERENCE:
71.10.00/04-G6
24 MO
MRB 8
711341-820-802
MRB REFERENCE:
71.10.00/05-G6
FNC
MEN
MRB REFERENCE:
71.10.00/01-G6
418AR
428AR
410 ENGINE COWLING
420
FUNCTIONAL CHECK OF FAN COWL LATCH TENSION.
SYSTEMS, APU AND POWER PLANT : POWER PLANT
24 MO
SOURCE
24 MO
OR
12000 FH
MRB 9
24 MO
MRB 9
711313-200-801
MRB REFERENCE:
71.13.00/01-RN
716100-220-801
MRB REFERENCE:
71.13.00/01-PW
24 MO
MRB 8
711300-720-802
MRB REFERENCE:
71.13.00/04-PW
FNC
I:
24 MO
MRB 8
711346-820-802
MRB REFERENCE:
71.12.00/04-RR
REV. DATE: JUL 01/21
SECTION:
2 -71
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
711300-R7-1
ZONE
412 FAN COWL
AF
422
GENERAL VISUAL INSPECTION FOR THE PRESENCE AND
SECURITY OF FAN COWL DOORS ZONE 1/AMBIENT SEALS.
ACCESS: 415AL
425AL
716000-N1-1
716000-N2-1
716000-N3-1
716100-R1-1
716100-R4-1
GVI
I: 10000 FH
MRB 8
REFERENCE
711300-200-811
416AR
426AR
I: 12000 FH
410 AIR INTAKE
AF
GVI
420
GENERAL VISUAL INSPECTION OF AIR INTAKE AEROFILLERS.
I: 12000 FH
410 AIR INTAKE
AF
420
GENERAL VISUAL INSPECTION OF AIR INTAKE OUTER
SURFACE.
I: 12000 FH
GVI
MRB 9
716041-210-802
MRB REFERENCE:
71.60.00/01-RN
MRB 9
716041-210-801
MRB REFERENCE:
71.60.00/02-RN
I:
412 AIR INTAKE COWL
AF
422
GENERAL VISUAL INSPECTION FOR THE PRESENCE AND
SECURITY OF NOSE COWL SEAL.
I: 12000 FH
MRB 9
716041-200-801
GVI
3200 FH
MRB 9
716141-200-802
410 POWERPLANT DRAINS
EN
VCK
420
VISUAL CHECK OF DRAINS LINES, MAST AND CONNECTIONS.
SYSTEMS, APU AND POWER PLANT : POWER PLANT
M/H
APPLICABILITY
1
1
0.30 TRENT 700
0.30
*
*
0.10
0.10
1
1
0.05 TRENT 7000
0.05
1
1
0.05 TRENT 7000
0.05
1
1
0.05 TRENT 7000
0.05
1
1
1.00 TRENT 700
1.00
1
1
0.30 TRENT 700
0.30
*
*
0.10
0.10
1
1
0.08 GE
0.08
MRB REFERENCE:
71.61.00/01-RR
MRB 9
716141-200-809
MRB REFERENCE:
71.61.00/02-RR
416AR
426AR
C O N T I N U E D
MEN
MRB REFERENCE:
71.60.00/03-RN
411 AIR INTAKE COWL
EN
GVI
421
GENERAL VISUAL INSPECTION OF THE AIRWASHED SURFACES
FOR DISTORTION AND SECURITY OF INSTALLATION.
* * * * *
SOURCE
MRB REFERENCE:
71.12.00/03-RR
410 AIR INTAKE
AF
GVI
420
GENERAL VISUAL INSPECTION OF NOSE LIP AND ACOUSTIC
LINER FOR EROSION.
ACCESS: 415AL
425AL
717000-G1-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
I:
12 MO
OR
6000 FH
MRB 9
717000-200-801
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-71
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
717000-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
*
0.20
0.20
APPLICABILITY
* * * * *
71.70.00/01-G6
ACCESS: 415AL
425AL
* * * * *
416AR
426AR
E N D
SYSTEMS, APU AND POWER PLANT : POWER PLANT
417AL
427AL
418AR
428AR
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -71
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
722000-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 FAN SECTION
EN
420
DISCARD LIFE LIMITED PARTS OF LP COMPRESSOR.
DIS
I:
NOTE
SOURCE
MRB 5
REFERENCE
722000-920-801
PREP.: ENGINE;
722100-G1-1
*
410 FAN SECTION
EN
420
DETAILED INSPECTION OF FAN BLADES AND SPINNER.
DET
I:
5000 FH
MRB 6
722200-R1-1
410 AIR INLET FAIRINGS
EN
420
DETAILED INSPECTION OF GAS GENERATOR FAIRING
COMPRESSOR, GAS GENERATOR COWLING UPPER SPLITTER
FAIRING, GAS GENERATOR COWLING-LOWER SPLITTER
FAIRING, AND FIRE SEALS.
DET
413 GAS GENERATOR FAIRINGS
AF
423
GENERAL VISUAL INSPECTION OF FAIRING AND PANELS.
GVI
ACCESS: 415AL
425AL
722200-R2-1
416AR
426AR
417AL
427AL
SYSTEMS, APU AND POWER PLANT : ENGINE
416AR
426AR
417AL
427AL
N/A GE
N/A
722100-210-804
36.00
1
1
0.30 GE
0.30
I: 12000 FH
MRB 8
722031-220-801
1
1
0.50 TRENT 7000
0.50
1
1
0.50 TRENT 700
0.50
*
*
0.20
0.20
1
1
0.50 TRENT 700
0.50
*
*
0.20
0.20
MRB REFERENCE:
72.21.00/01-RN
I: 12000 FH
MRB 9
722241-200-803
MRB REFERENCE:
72.03.00/01-RR
418AR
428AR
413 GAS GENERATOR FAIRINGS
AF
GVI
423
GENERAL VISUAL INSPECTION OF SPLITTER FAIRING FIRE
SEALS.
ACCESS: 415AL
425AL
APPLICABILITY
MRB REFERENCE:
72.20.00/01-G6
NOTE:
ETOPS RELEVANT
722100-N1-1
0
0
M/H
MRB REFERENCE:
72.20.00/02-G6
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
R
MEN
I: 12000 FH
MRB 8
722241-200-804
MRB REFERENCE:
72.03.00/02-RR
418AR
428AR
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
723000-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 HIGH PRESSURE COMPRESSOR
420
DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR
(OFF-AIRCRAFT).
EN
DIS
I:
NOTE
SOURCE
MRB 5
REFERENCE
723000-920-801
MEN
0
0
M/H
APPLICABILITY
N/A GE
N/A
MRB REFERENCE:
72.30.00/01-G6
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
723100-N1-1
*
410 LP COMPRESSOR MODULE
EN
420
LUBRICATION OF LP COMPRESSOR BLADE DOVETAIL ROOT
FLANKS AND LP COMPRESSOR DISC POSTS
LUB
I: 10000 FC
MRB 5
723534-640-801
36.00
2
2
3.00 TRENT 7000
3.00
1
1
1.00 TRENT 7000
1.00
0
0
N/A TRENT 7000
N/A
MRB REFERENCE:
72.31.00/01-RN
NOTE:
ETOPS RELEVANT
723100-N2-1
410 LP COMPRESSOR MODULE
420
DETAILED INSPECTION OF LP COMPRESSOR BLADES
EN
DET
I:
7500 FH
MRB 6
MRB REFERENCE:
72.31.00/02-RN
NOTE:
ETOPS RELEVANT
723100-N3-1
410 LP COMPRESSOR MODULE
EN
DIS
420
DISCARD LP COMPRESSOR DISC AND SHAFT (OFF-AIRCRAFT)
723113-220-803
I:
NOTE
MRB 5
723534-920-801
MRB REFERENCE:
72.31.00/03-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
SYSTEMS, APU AND POWER PLANT : ENGINE
*
REV. DATE: JUL 01/21
SECTION:
2 -72
64.00
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
723100-N4-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 LP COMPRESSOR MODULE
EN
DET
420
DETAILED INSPECTION OF LP COMPRESSOR BLADES LEADING
EDGE FOR DEFORMATION.
I:
NOTE
SOURCE
MRB 6
REFERENCE
723113-220-801
MEN
M/H
APPLICABILITY
1
1
3.85 TRENT 7000
3.85
0
0
N/A TRENT 7000
N/A
MRB REFERENCE:
72.31.00/04-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
723100-N5-1
410 LP COMPRESSOR MODULE
EN
RST
420
RESTORE COATING TO LP COMPRESSOR BLADE DOVETAIL ROOT
FLANKS (OFF-AIRCRAFT)
I: 10000 FC
MRB 6
723113-300-801
MRB REFERENCE:
72.31.00/05-RN
NOTE:
ETOPS RELEVANT
PREP.: ENGINE REMOVED;
723100-P1-1
410 LOW PRESSURE COMPRESSOR GROUP
420
DETAILED INSPECTION OF FAN BLADES.
*
EN
DET
I:
2100 FH
MRB 6
410 LOW PRESSURE COMPRESSOR GROUP
EN
DIS
420
DISCARD FAN HUB AND LPC DRUM ROTOR (OFF-AIRCRAFT).
1
1
0.25 PW
0.25
0
0
N/A PW
N/A
MRB REFERENCE:
72.31.00/01-PW
NOTE:
ETOPS RELEVANT
723100-P3-1
723112-200-801
64.00
I:
NOTE
MRB 5
723100-920-801
MRB REFERENCE:
72.31.00/03-PW
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
SYSTEMS, APU AND POWER PLANT : ENGINE
*
REV. DATE: JUL 01/21
SECTION:
2-72
36.00
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
723100-P6-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 LOW PRESSURE COMPRESSOR GROUP
EN
420
LUBRICATION OF 1ST STAGE LOW PRESSURE COMPRESSOR
(LPC) BLADE ASSEMBLY (FAN BLADE) ROOT.
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
LUB
I:
2500 FC
NOTE
MRB 6
MRB REFERENCE:
72.31.00/06-PW
1
1
TBD PW
TBD
DET
I:
1600 FH
MRB 6
723141-200-801
1
1
0.87 TRENT 700
0.87
0
0
N/A TRENT 700
N/A
NOTE:
- ETOPS RELEVANT
- INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH
OPERATOR EXPERIENCE
723100-R1-1
411 LP COMPRESSOR MODULE
EN
421
DETAILED INSPECTION OF LP COMPRESSOR BLADES.
MRB REFERENCE:
72.31.00/01-RR
NOTE:
ETOPS RELEVANT
723100-R2-1
410 LP COMPRESSOR MODULE
EN
420
DISCARD LIFE LIMITED PARTS OF THE LP COMPRESSOR
(OFF-AIRCRAFT).
DIS
I:
NOTE
MRB 5
723151-920-801
MRB REFERENCE:
72.31.00/02-RR
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
723100-R7-1
411 LP COMPRESSOR MODULE
EN
LUB
421
RE-LUBRICATION OF LP COMPRESSOR BLADE ROOT COATINGS.
*
I:
1200 FC
MRB 6
723141-300-802
2
2
3.00 TRENT 700
3.00
*
8.00
MRB REFERENCE:
72.31.00/03-RR
NOTE:
ETOPS RELEVANT
PREP.: LP COMPRESSOR BLADES Z410;
LP COMPRESSOR BLADES Z420;
SYSTEMS, APU AND POWER PLANT : ENGINE
36.00
REV. DATE: JUL 01/21
SECTION:
2-72
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
D
723112-P1-1
R
723200-G1-1
ZONE
SOURCE
REFERENCE
MEN
VSB ROHR
CF6-80E1-NAC-71039
1
1
CMP REFERENCE:
72-2-0104-003
*
*
723200-920-802
0
0
M/H
APPLICABILITY
************** TASK DELETED **************
410 ENGINE BLEED SYSTEM
EN
CHK
420
INSPECTION AND RIGGING OF BLEED SYSTEM COMPONENTS
ACCESS: 416AR
426AR
723200-N1-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
I:
2000 FH
CMP
VSB
418AR
428AR
410 IP COMPRESSOR MODULE
EN
420
DISCARD IP COMPRESSOR ROTOR DRUM (OFF-AIRCRAFT).
DIS
I:
NOTE
MRB 5
2.50 GE
2.50 ETOPS
PRE 55252
PRE VSB CF60.10 80E1-NAC-36-003
0.10
N/A TRENT 7000
N/A
MRB REFERENCE:
72.32.00/01-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
723200-P1-1
*
410 LPC / LPT COUPLING GROUP
420
DISCARD LPC/LPT COUPLING (OFF-AIRCRAFT).
EN
DIS
I:
NOTE
MRB 5
723200-920-801
0
0
64.00
N/A PW
N/A
MRB REFERENCE:
72.32.00/01-PW
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
723200-R1-1
*
410 IP COMPRESSOR MODULE
EN
420
DISCARD LIFE LIMITED PARTS OF THE IP COMPRESSOR
(OFF-AIRCRAFT).
DIS
I:
NOTE
MRB 5
723000-920-802
0
0
36.00
N/A TRENT 700
N/A
MRB REFERENCE:
72.32.00/01-RR
72.33.00/01-RR
NOTE:
- ETOPS RELEVANT
INTERVAL:
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
723200-R1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
36.00
APPLICABILITY
* * * * *
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
723300-N1-1
410 COMPRESSOR INTERMEDIATE MODULE
EN
DIS
420
DISCARD IP COMPRESSOR REAR STUB SHAFT (OFF-AIRCRAFT).
I:
NOTE
MRB 6
723300-920-801
0
0
N/A TRENT 7000
N/A
MRB REFERENCE:
72.33.00/01-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
723300-P2-1
412 FAN CASE GROUP
AF
422
GENERAL VISUAL INSPECTION OF FAN CASE, ACOUSTIC
LINERS AND FAN EXIT GUIDE VANES.
ACCESS: 415AL
425AL
723400-R3-1
723500-P1-1
415AR
425AR
416AR
426AR
GVI
I: 10000 FH
MRB 9
723300-210-801
MRB REFERENCE:
72.33.00/02-PW
416BR
426BR
410 LP COMPRESSOR CASING
EN
GVI
420
GENERAL VISUAL INSPECTION OF THE FAN TRACK AND COLD
STREAM DUCT, AS FAR AS VISIBLE FROM THE FRONT, FOR
SIGNIFICANT DAMAGE.
I:
410 HIGH PRESSURE COMPRESSOR (HPC)
420
DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR
(OFF-AIRCRAFT).
I:
EN
DIS
1000 FH
MRB 9
722100-200-805
MRB REFERENCE:
72.34.00/01-RR
NOTE
MRB 5
723500-920-801
MRB REFERENCE:
72.35.00/01-PW
1
1
0.50 PW
0.50
*
*
0.17
0.17
1
1
0.25 TRENT 700
0.25
0
0
N/A PW
N/A
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
723500-P1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
M/H
*
36.00
APPLICABILITY
* * * * *
PREP.: ENGINE;
724000-G1-1
MEN
413 COMBUSTION SECTION
NDT SDI
423
BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER AND
DOME.
I:
500 FC
OR
2000 FH
MRB 8
720000-290-808
1
1
3.00 GE
3.00
*
*
0.20
0.20
1
1
1.20 TRENT 7000
1.20
1
1
0.90 TRENT 7000
0.90
1
1
3.00 PW
3.00
MRB REFERENCE:
72.40.00/01-G6
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
724000-N1-1
416AR
426AR
417AL
427AL
418AR
428AR
410 COMBUSTION SECTION
NDT SDI
420
SPECIAL DETAILED INSPECTION OF COMBUSTOR HEAD
SECTION, FUEL SPRAY NOZZLES HEAD SECTION, COMBUSTION
LINER TILES, REAR INNER COMBUSTION LINER AND REAR
OUTER COMBUSTION LINER.
T:
9000 FH
OR
1000 FC
I:
1000 FC
OR
4500 FH
T:
9000 FH
OR
1000 FC
MRB 6,9
720000-290-839
MRB REFERENCE:
72.40.00/01-RN
NOTE:
ETOPS RELEVANT
724000-N2-1
410 COMBUSTION SECTION
NDT
420
SPECIAL DETAILED INSPECTION OF HP TURBINE NOZZLE
GUIDE VANES.
SDI
NOTE:
ETOPS RELEVANT
R
724100-P1-1
413 DIFFUSER, COMBUSTION & TURBINE NOZZLE GROUP NDT SDI
423
BORESCOPE INSPECTION OF INNER AND OUTER COMBUSTION
CHAMBER ASSEMBLIES AND FIRST STAGE VANES.
I:
4500 FH
OR
1000 FC
I:
700 FC
OR
2400 FH
MRB 6
720000-290-843
MRB REFERENCE:
72.40.00/02-RN
MRB 8
720000-290-832
MRB REFERENCE:
72.41.00/01-PW
NOTE:
ETOPS RELEVANT
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-72
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
724100-P1-1
ZONE
* * * * *
C O N T I N U E
ACCESS: 415BL
425BL
724100-R1-1
416BR
426BR
417AL
427AL
416AR
426AR
417AL
427AL
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.13
0.13
1
1
1.50 TRENT 700
1.50
*
*
0.20
0.20
* * * * *
418AR
428AR
410 COMBUSTION SECTION
420
BORESCOPE INSPECTION OF COMBUSTION LINER
ACCESS: 415AL
425AL
724120-N1-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
NDT
SDI
I:
1500 FC
OR
6000 FH
MRB 9
MRB REFERENCE:
72.41.00/01-RR
418AR
428AR
410 HP COMPRESSOR ASSY
420
DISCARD HP COMRESSOR ROTOR DRUM ASSEMBLIES
(OFF-AIRCRAFT)
EN
DIS
I:
NOTE
720000-200-818
MRB 5
724100-920-801
MRB REFERENCE:
72.41.20/01-RN
0
0
N/A TRENT 7000
N/A
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
724120-R1-1
*
410 HP COMPRESSOR SECTION
EN
420
DISCARD LIFE LIMITED PARTS OF THE HP COMPRESSOR
(OFF-AIRCRAFT).
DIS
I:
NOTE
MRB 5
723000-920-803
0
0
64.00
N/A TRENT 700
N/A
MRB REFERENCE:
72.41.20/01-RR
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
724150-N1-1
*
410 HP TURBINE ASSY
420
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
EN
DIS
I:
NOTE
MRB 5
725000-920-811
0
0
36.00
N/A TRENT 7000
N/A
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
724150-N1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
64.00
APPLICABILITY
* * * * *
DISCARD HP TURBINE DISC AND HP TURBINE FRONT COVER
PLATE (OFF-AIRCRAFT)
MRB REFERENCE:
72.41.50/01-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
724150-N2-1
724150-R1-1
410 HP TURBINE ASSY
EN
SDI
420
SPECIAL DETAILED BORESCOPE INSPECTION OF HP TURBINE
BLADES
410 HP TURBINE SECTION
NDT
420
BORESCOPE INSPECTION OF HP TURBINE NOZZLE GUIDE
VANES.
SDI
T:
I:
4500 FH
OR
1000 FC
T:
2000 FC
OR
8500 FH
I:
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
724150-R2-1
416AR
426AR
417AL
427AL
NOTE:
ETOPS RELEVANT
SYSTEMS, APU AND POWER PLANT : ENGINE
NDT
SDI
T:
I:
416AR
426AR
417AL
427AL
MRB 6,9
720000-290-842
MRB 6
2.00 TRENT 7000
2.00
720000-200-817
1
1
2.00 TRENT 700
2.00
*
*
0.20
0.20
1
1
0.75 TRENT 700
0.75
*
*
0.20
0.20
MRB REFERENCE:
72.41.50/01-RR
1500 FC
OR
6000 FH
2000 FC
OR
8500 FH
1
1
MRB REFERENCE:
72.41.50/02-RN
418AR
428AR
410 HP TURBINE SECTION
420
BORESCOPE INSPECTION OF HP TURBINE BLADES.
ACCESS: 415AL
425AL
9000 FH
OR
1000 FC
MRB 6
720000-200-814
MRB REFERENCE:
72.41.50/02-RR
1500 FC
OR
6000 FH
418AR
428AR
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
724150-R3-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 HP TURBINE SECTION
EN
420
DISCARD LIFE LIMITED PARTS OF THE HP TURBINE
(OFF-AIRCRAFT).
DIS
I:
NOTE
SOURCE
MRB 5
REFERENCE
725000-920-805
MEN
0
0
M/H
APPLICABILITY
N/A TRENT 700
N/A
MRB REFERENCE:
72.41.50/03-RR
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
725000-G1-1
*
413 TURBINE SECTION
EN
DIS
423
DISCARD LIFE LIMITED PARTS OF HPT AND LPT ROTORS.
I:
NOTE
MRB 5
725000-920-802
0
0
36.00
N/A GE
N/A
MRB REFERENCE:
72.50.00/02-G6
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
725100-N1-1
*
410 IP TURBINE MODULE
EN
420
DISCARD IP TURBINE DISC AND IP TURBINE SHAFT
(OFF-AIRCRAFT)
DIS
I:
NOTE
MRB 5
725100-920-801
0
0
36.00
N/A TRENT 7000
N/A
MRB REFERENCE:
72.51.00/01-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
725100-R1-1
*
410 IP TURBINE MODULE
EN
420
DISCARD LIFE LIMITED PARTS OF THE IP TURBINE
(OFF-AIRCRAFT).
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
DIS
I:
NOTE
MRB 5
725000-920-806
MRB REFERENCE:
72.51.00/01-RR
0
0
64.00
N/A TRENT 700
N/A
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
725100-R1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
36.00
APPLICABILITY
* * * * *
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
725200-G1-1
413 HIGH PRESSURE TURBINE ROTOR ASSY
NDT
423
BORESCOPE INSPECTION OF STAGE 1 AND STAGE 2 HP
TURBINE BLADES.
SDI
I:
500 FC
OR
2400 FH
MRB 6
720000-290-809
MRB REFERENCE:
72.50.00/01-G6
1
1
0.60 GE
0.60
*
*
0.20
0.20
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
725200-N1-1
416AR
426AR
417AL
427AL
418AR
428AR
410 LP TURBINE MODULE
EN
DIS
420
DISCARD LP TURBINE DISC STAGES 1 TO 6 AND LP TURBINE
SHAFT (OFF-AIRCRAFT)
I:
NOTE
MRB 5
725200-920-802
0
0
N/A TRENT 7000
N/A
MRB REFERENCE:
72.52.00/01-RN
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE REMOVED;
725200-P1-1
*
413 HIGH PRESSURE TURBINE GROUP
NDT SDI
423
BORESCOPE INSPECTION OF THE FIRST AND SECOND STAGE
HIGH PRESSURE TURBINE BLADES.
I:
700 FC
OR
2400 FH
MRB 6
720000-290-835
MRB REFERENCE:
72.52.00/01-PW
1
1
64.00
0.60 PW
0.60
NOTE:
ETOPS RELEVANT
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
725200-P1-1
ZONE
* * * * *
C O N T I N U E
ACCESS: 415BL
425BL
725200-P2-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
416BR
426BR
417AL
427AL
SOURCE
REFERENCE
MEN
M/H
*
*
0.13
0.13
APPLICABILITY
* * * * *
418AR
428AR
410 HIGH PRESSURE TURBINE GROUP
420
DISCARD LIFE LIMITED PARTS OF HP TURBINE
(OFF-AIRCRAFT).
EN
DIS
I:
NOTE
MRB 5
725200-920-801
0
0
N/A PW
N/A
MRB REFERENCE:
72.52.00/02-PW
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
725200-P3-1
*
413 HIGH PRESSURE TURBINE GROUP
NDT SDI
423
BORESCOPE INSPECTION OF SECOND STAGE HIGH PRESSURE
TURBINE VANES
T:
NOTE
I:
NOTE
I:
NOTE
CMP
VSB
VSB
PW4G-100-72-195
1
1
36.00
3.00 PW
3.00 PRE
SB PW 72-206
CMP REFERENCE:
72-2-0204-007
NOTE:
- REFER TO VSB PW4G-100-72-195 FOR THRESHOLD AND
INTERVAL
725200-R1-1
410 LP TURBINE SECTION
EN
420
DISCARD LIFE LIMITED PARTS OF THE LP TURBINE
(OFF-AIRCRAFT).
DIS
MRB 5
725000-920-807
0
0
N/A TRENT 700
N/A
MRB REFERENCE:
72.52.00/01-RR
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
SYSTEMS, APU AND POWER PLANT : ENGINE
*
REV. DATE: JUL 01/21
SECTION:
2-72
36.00
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
725300-P1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 LOW PRESSURE TURBINE GROUP
420
DISCARD LIFE LIMITED PARTS OF LP TURBINE
(OFF-AIRCRAFT).
EN
DIS
I:
NOTE
SOURCE
MRB 5
REFERENCE
725300-920-801
MEN
0
0
M/H
APPLICABILITY
N/A PW
N/A
MRB REFERENCE:
72.53.00/01-PW
NOTE:
- ETOPS RELEVANT
INTERVAL:
- FOR INTERVAL REFER TO CHAPTER 5 OF ENGINE SHOP
MANUAL (ESM)(GE AND PW) OR TIME LIMITS MANUAL (RR)
PREP.: ENGINE;
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE
E N D
*
36.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -72
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
731000-N1-1
731000-P1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 FUEL DISTRIBUTION
420
DISCARD LP FUEL FILTER ELEMENT
EN
413 FUEL DISTRIBUTION
423
DISCARD FUEL FILTER ELEMENT.
EN
DIS
I:
6000 FH
SOURCE
MRB 6
REFERENCE
731113-920-801
MEN
M/H
APPLICABILITY
1
1
0.58 TRENT 7000
0.58
1
1
0.15 PW
0.15
*
*
0.07
0.07
1
1
0.35 TRENT 700
0.35
*
*
0.10
0.10
1
1
0.20 GE
0.20
MRB REFERENCE:
73.10.00/01-RN
DIS
I:
5000 FH
NOTE
MRB 6
731100-920-801
MRB REFERENCE:
73.10.00/01-PW
NOTE:
- DISCARD FUEL FILTER ELEMENT AT 150 FH, 800 FH AND
1600 FH AFTER AIRCRAFT DELIVERY THEREAFTER EVERY
5000 FH
- DISCARD FUEL FILTER ELEMENT AT 150 FH AND 800 FH
AFTER MAJOR TANK INTERVENTION THEREAFTER EVERY 5000
FH.
- ETOPS RELEVANT
ACCESS: 416BR
426BR
731000-R1-1
418AR
428AR
410 FUEL DISTRIBUTION
420
DISCARD LP FUEL FILTER ELEMENT.
EN
DIS
I:
6000 FH
NOTE
MRB 9
MRB REFERENCE:
73.10.00/01-RR
NOTE:
- DISCARD FUEL FILTER ELEMENT AT 150 FH, 800 FH AND
1600 FH AFTER AIRCRAFT DELIVERY THEREAFTER EVERY 6000
FH
- DISCARD FUEL FILTER ELEMENT AT 150 FH AND 800 FH
AFTER MAJOR TANK INTERVENTION THEREAFTER EVERY 6000
FH.
ACCESS: 415AL
425AL
731110-G1-1
416AR
426AR
410 ENGINE FUEL AND CONTROL - GENERAL
420
DISCARD FUEL FILTER
EN
DIS
I:
6000 FH
NOTE
MRB 9
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ENGINE FUEL AND CONTROL
731142-920-801
MRB REFERENCE:
73.00.00/01-G6
NOTE:
- DISCARD FUEL FILTER ELEMENT AT 150 FH, 800 FH AND
* * * * *
731141-920-801
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -73
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
731110-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
*
0.10
0.10
APPLICABILITY
* * * * *
1600 FH AFTER AIRCRAFT DELIVERY THEREAFTER EVERY 6000
FH
- DISCARD FUEL FILTER ELEMENT AT 150 FH AND 800 FH
AFTER MAJOR TANK INTERVENTION THEREAFTER EVERY 6000
FH.
ACCESS: 416AR
426AR
N
732000-P1-1
418AR
428AR
210 FUEL CONTROL
EN
OPC
I:
1000 FH
MRB 9
READ SMR FOR CHANNEL A AND B FAULTS.
732100-N1-1
732100-N2-1
EN
410 ENGINE CONTROL AND FAULT MONITORING
420
DRY THE P30 PRESSURE SENSOR MANIFOLD
EN
E N D
1
TBD PW
MRB REFERENCE:
73.20.00/01-PW
410 ENGINE CONTROL AND FAULT MONITORING
420
DRAIN THE PS26 SENSE LINE MOISTURE TRAP
* * * * *
732100-710-821
RST
I:
550 FC
MRB 6
732147-680-801
1
1
0.20 TRENT 7000
0.20
1
1
0.60 TRENT 7000
0.60
MRB REFERENCE:
73.21.00/01-RN
RST
I:
550 FC
MRB 7
732147-200-801
MRB REFERENCE:
73.21.00/02-RN
* * * * *
SYSTEMS, APU AND POWER PLANT : ENGINE FUEL AND CONTROL
REV. DATE: JUL 01/21
SECTION:
2 -73
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
753300-N1-1
753300-N2-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 AIR BLEED SYSTEM
420
DETAILED INSPECTION OF HP BLEED VALVE SEAL
EN
410 AIR BLEED SYSTEM
420
DETAILED INSPECTION OF IP BLEED VALVE SEAL
EN
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : ENGINE - AIR
DET
I: 12000 FH
SOURCE
MRB 8
REFERENCE
753317-200-801
MEN
M/H
APPLICABILITY
1
1
0.10 TRENT 7000
0.10
1
1
0.15 TRENT 7000
0.15
MRB REFERENCE:
75.33.00/01-RN
DET
I: 30000 FH
MRB 8
753316-200-801
MRB REFERENCE:
75.33.00/02-RN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-75
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
771300-P1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 ENGINE PRESSURE RATIO (EPR) INDICATING SYSTEMEN
420
INSPECTION AND CLEANING OF CONDENSATION TRAP
ASSEMBLIES (WATER TRAPS), FOR OBSTRUCTIONS OR
BLOCKAGE
ACCESS: 415BL
425BL
* * * * *
CHK
I:
1000 FC
SOURCE
CMP
MAN
REFERENCE
MAN
PW4G-100-2-00
SYSTEMS, APU AND POWER PLANT : ENGINE INDICATING
M/H
1
1
1.00 PW
1.00
*
*
0.06
0.06
APPLICABILITY
CMP REFERENCE:
72-2-0204-009
417AL
427AL
E N D
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-77
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
781000-N1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 EXHAUST COLLECTOR/NOZZLE
420
DETAILED INSPECTION OF FINGER SEALS.
EN
DET
I: 12000 FH
SOURCE
MRB 8
R
781100-R1-1
410 EXHAUST COLLECTOR/NOZZLE
EN
DET
420
DETAILED INSPECTION OF EXHAUST NOZZLE WEAR PLATE.
I: 12000 FH
410 EXHAUST COLLECTOR/NOZZLE
EN
420
GENERAL VISUAL INSPECTION OF EXHAUST NOZZLE FIRE
SEALS.
I:
ACCESS: 415AL
425AL
783100-G1-1
416AR
426AR
417AL
427AL
* * * * *
SYSTEMS, APU AND POWER PLANT : EXHAUST
781242-220-801
EN
2000 FH
MRB 8
781100-200-802
RST
I:
6000 FC
MRB 6
783141-600-801
DET
I:
18 MO
OR
1650 FC
MRB 6
122278-600-802
417AL
LUB
I:
1000 FC
MRB 6
122278-600-801
0.50 TRENT 7000
0.50
TBD
1
1
0.05 TRENT 7000
0.05
1
1
0.50 TRENT 700
0.50
*
*
0.20
0.20
1
1
0.10 GE
0.10
*
*
0.20
0.20
1
1
0.50 GE
0.50
*
*
0.10
0.10
1
1
0.50 GE
0.50
*
0.20
MRB REFERENCE:
78.31.00/03-G6
418AR
C O N T I N U E D
*
APPLICABILITY
MRB REFERENCE:
78.31.00/02-G6
416AR
426AR
416AR
1
1
M/H
MRB REFERENCE:
78.11.00/01-RR
MRB REFERENCE:
78.31.00/01-G6
EN
MEN
MRB REFERENCE:
78.10.00/02-RN
418AR
428AR
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
420
LUBRICATE BALLSCREW ACTUATORS.
ACCESS: 415AL
GVI
MRB 9
418AR
428AR
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
EN
420
DETAILED INSPECTION AND LUBRICATE FLEXIBLE DRIVE
SHAFTS.
ACCESS: 415AL
425AL
783100-G3-1
417AL
427AL
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
420
REMOVE AND REPACK ANGLE GEARBOX.
ACCESS: 415AL
425AL
783100-G2-1
416AR
426AR
781241-220-801
MRB REFERENCE:
78.10.00/01-RN
PREP.: FAN COWL OPEN;
THRUST REVERSER COWL OPEN;
781000-N2-1
REFERENCE
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-78
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
783100-G3-1
ZONE
* * * * *
425AL
783100-G5-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
426AR
427AL
SOURCE
REFERENCE
MEN
M/H
*
0.20
1
1
0.25 GE
0.25
*
*
0.20
0.20
1
1
0.50 GE
0.50
*
*
0.10
0.10
1
1
0.50 GE
0.50
*
*
0.10
0.10
APPLICABILITY
* * * * *
428AR
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
EN
DET
420
DETAILED INSPECTION OF TRANSCOWL INNER BONDMENT SEAL
AND MATING SURFACES (FORWARD FAIRING AND AFT FRAME
ASSEMBLY).
I:
4 C
NOTE
MRB 9
783100-210-801
MRB REFERENCE:
78.31.00/05-G6
NOTE:
- TASK CAN BE ACCOMPLISHED AT OPPORTUNITY OF THRUST
REVERSER REMOVAL.
ACCESS: 415AL
425AL
783100-G6-1
416AR
426AR
417AL
427AL
418AR
428AR
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
420
HOLDING TORQUE CHECK OF THE CDU CONE BRAKE.
EN
FNC
I:
4 C
NOTE
MRB 9
783143-720-801
MRB REFERENCE:
78.31.00/04-G6
NOTE:
- TASK CAN BE ACCOMPLISHED AT OPPORTUNITY OF THRUST
REVERSER REMOVAL.
ACCESS: 415AL
425AL
783100-G7-1
416AR
426AR
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
420
HOLDING TORQUE CHECK OF THE THRUST REVERSER
ELECTROMECHANICAL BRAKE.
EN
FNC
I:
9000 FH
NOTE
MRB 9
783751-720-801
MRB REFERENCE:
78.31.00/06-G6
NOTE:
- TASK CAN BE ACCOMPLISHED AT OPPORTUNITY OF THRUST
REVERSER REMOVAL.
ACCESS: 415AL
425AL
SYSTEMS, APU AND POWER PLANT : EXHAUST
416AR
426AR
REV. DATE: JUL 01/21
SECTION:
2 -78
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
783100-N1-1
783154-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 THRUST REVERSER CONTROL AND INDICATING
EN
OPC
420
OPERATIONAL CHECK OF THRUST REVERSER PRIMARY LOCKING
SYSTEM WITH SYNCHRO SHAFTS.
I: 40000 FH
410 THRUST REVERSER CONTROL/ACTUATION SYSTEM
EN
CHK
420
THRUST REVERSER DIRECTIONAL PILOT VALVE LEAK CHECK.
I: 12000 FH
SOURCE
CMR*
REFERENCE
783105-710-802
783200-G6-1
1
1
1.00 GE
1.00
*
*
0.05
0.05
1
1
0.25 GE
0.25
PREP.: THRUST REVERSER DEPLOYED;
*
0.20
ACCESS: 415AL
425AL
*
*
0.20
0.20
1
1
0.20 GE
0.20
*
*
0.20
0.20
1
1
0.30 GE
0.30
*
*
0.20
0.20
1
1
1.18 TRENT 7000
1.18
410 THRUST REVERSER ASSEMBLY
EN
DET
420
DETAILED INSPECTION OF: . BLOCKER DOORS, HINGES AND
ADJACENT STRUCTURE . FAN REVERSER DEFLECTION.
416AR
426AR
417AL
427AL
CMR REFERENCE:
783100-00001-1-C
MRB 9
783154-790-801
MRB REFERENCE:
78.31.00/07-G6
416AR
426AR
417AL
427AL
EN
GVI
417AL
427AL
SYSTEMS, APU AND POWER PLANT : EXHAUST
MRB 9
783200-210-802
MRB REFERENCE:
78.32.00/01-G6
78.32.00/02-G6
I:
18 MO
MRB 8
783200-210-810
418AR
428AR
I:
18 MO
MRB 8
783200-210-809
MRB REFERENCE:
78.32.00/07-G6
418AR
428AR
410 THRUST REVERSER STRUCTURE
EN
420
DETAILED INSPECTION OF CASCADES, BLOCKER DOORS,
* * * * *
18 MO
MRB REFERENCE:
78.32.00/06-G6
410 THRUST REVERSER ASSEMBLY
EN
GVI
420
GENERAL VISUAL INSPECTION OF FIRE PROTECTION COATING.
416AR
426AR
I:
418AR
428AR
410 THRUST REVERSER ASSEMBLY
420
GENERAL VISUAL INSPECTION OF REVERSER
FIRESHIELD/SEALS.
ACCESS: 415AL
425AL
783200-N1-1
APPLICABILITY
0.05 A330-800
0.05 OR
A330-900
ACCESS: 415AL
425AL
783200-G7-1
M/H
1
1
ACCESS: 415AL
425AL
783200-G2-1
MEN
C O N T I N U E D
DET
I:
2200 FC
OR
12000 FH
MRB 9
783242-220-801
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -78
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
783200-N1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF THERMAL BLANKET AND FIRE
SHIELDS.
I: 12000 FH
MRB 8
783200-210-814
783200-N5-1
410 THRUST REVERSER STRUCTURE
EN
420
OPERATIONAL CHECK OF PRESSURE RELIEF LATCHES.
OPC
410 THRUST REVERSER STRUCTURE
EN
420
GENERAL VISUAL INSPECTION OF PRESSURE SEALS.
GVI
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF FIXED STRUCTURE FIRE
SEALS.
I:
48 MO
OR
24000 FH
MRB 8
2500 FC
OR
12000 FH
MRB 9
I: 12000 FH
OR
24 MO
MRB 8
I:
783218-710-801
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF TRANSCOWL LOCATORS WEAR
PADS.
783248-210-801
MRB REFERENCE:
78.32.00/04-RN
783200-210-813
MRB REFERENCE:
78.32.00/05-RN
I: 10000 FC
MRB 9
783211-210-815
1
1
0.93 TRENT 7000
0.93
*
1.00
1
1
0.33 TRENT 7000
0.33
1
1
0.33 TRENT 7000
0.33
1
1
0.95 TRENT 7000
0.95
*
1.00
1
1
0.20 TRENT 7000
0.20
*
1.00
MRB REFERENCE:
78.32.00/06-RN
PREP.: FAN COWL OPEN AND T/R OPEN;
SYSTEMS, APU AND POWER PLANT : EXHAUST
1.00
MRB REFERENCE:
78.32.00/03-RN
PREP.: FAN COWL OPEN AND T/R OPEN;
783200-N6-1
*
MRB REFERENCE:
78.32.00/02-RN
PREP.: FAN COWL OPEN AND T/R OPEN;
783200-N4-1
APPLICABILITY
78.32.00/01-RN
PREP.: FAN COWL OPEN AND T/R OPEN;
783200-N3-1
M/H
* * * * *
BLOCKER DOORS MECHANISMS, SLAT CLEARANCE PANEL AND
THE INNER FACE OF THE TRANSCOWL EXTERNAL PANEL.
783200-N2-1
MEN
REV. DATE: JUL 01/21
SECTION:
2-78
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
783200-N7-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF REAR MOUNT FAIRING SEAL
LANDING.
I: 12000 FH
SOURCE
MRB 9
REFERENCE
783246-210-801
*
1.00
1
1
0.50 PW
0.50
*
*
0.23
0.23
1
1
0.50 PW
0.50
*
*
0.23
0.23
1
1
1.50 TRENT 700
1.50
PREP.: THRUST REVERSER DEPLOYED;
*
0.20
ACCESS: 415AL
425AL
*
*
0.10
0.10
1
1
0.75 TRENT 700
0.75
*
*
0.20
0.20
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF FIXED STRUCTURE SEALS.
783201-R1-1
415BL
425BL
416AR
426AR
416BR
426BR
417AL
427AL
410 THRUST REVERSER STRUCTURE
420
GENERAL VISUAL INSPECTION OF FIRE BLANKET.
ACCESS: 415AL
425AL
783200-R3-1
APPLICABILITY
0.20 TRENT 7000
0.20
ACCESS: 415AL
425AL
783200-P4-1
M/H
1
1
MRB REFERENCE:
78.32.00/07-RN
PREP.: FAN COWL OPEN AND T/R OPEN;
783200-P3-1
MEN
415BL
425BL
416AR
426AR
416BR
426BR
417AL
427AL
EN
MRB 8
783000-210-807
MRB REFERENCE:
78.32.00/03-PW
GVI
I:
24 MO
MRB 8
783000-210-808
MRB REFERENCE:
78.32.00/04-PW
418AR
428AR
I:
6000 FH
MRB 9
783200-200-804
MRB REFERENCE:
78.32.00/06-RR
416AR
426AR
410 THRUST REVERSER STRUCTURE
EN
420
GENERAL VISUAL INSPECTION OF THE INNER FIXED
STRUCTURE FIRE SEALS.
SYSTEMS, APU AND POWER PLANT : EXHAUST
18 MO
418AR
428AR
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF THE PIVOT DOOR DEFLECTOR
PLATES, MOVEABLE PANELS AND MECHANISM (THRUST
REVERSER DEPLOYED).
ACCESS: 415AL
425AL
I:
416AR
426AR
417AL
427AL
GVI
I:
24 MO
OR
12000 FH
MRB 8
783200-200-817
MRB REFERENCE:
78.32.00/05-RR
418AR
428AR
REV. DATE: JUL 01/21
SECTION:
2-78
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
783201-R2-1
ZONE
410 THRUST REVERSER STRUCTURE
EN
GVI
420
GENERAL VISUAL INSPECTION OF FRONT FRAME AND INNER
FIXED STRUCTURE THERMAL BLANKETS.
ACCESS: 415AL
425AL
783201-R5-1
783700-R1-1
416AR
426AR
417AL
427AL
I:
I: 12000 FH
MRB 9
783200-200-821
416AR
426AR
410 THR REVERSER INDEPENDANT LOCKING SYS
EN
420
OPERATIONAL CHECK OF THE SECONDARY AND TERTIARY
LOCKS.
I:
SYSTEMS, APU AND POWER PLANT : EXHAUST
783200-200-818
MRB REFERENCE:
78.32.00/01-RR
I:
* * * * *
MRB 8
REFERENCE
OPC
5000 FC
OR
24000 FH
MRB 8
48 MO
OR
4600 FC
MRB 9
783753-220-801
M/H
APPLICABILITY
1
1
0.75 TRENT 700
0.75
*
*
0.20
0.20
1
1
0.20 TRENT 700
0.20
*
*
0.10
0.10
1
1
0.27 TRENT 7000
0.27
1
1
1.00 TRENT 700
1.00
*
*
0.10
0.10
MRB REFERENCE:
78.37.00/01-RN
783700-710-801
MRB REFERENCE:
78.32.00/08-RR
78.37.00/01-RR
416AR
426AR
E N D
MEN
MRB REFERENCE:
78.32.00/07-RR
410 THRUST REVERSER INDEPENDENT LOCKING SYSTEM
EN
DET
420
DETAILED INSPECTION OF TERTIARY LOCK SYSTEM ROLLER.
ACCESS: 415AL
425AL
1600 FH
SOURCE
418AR
428AR
410 THRUST REVERSER STRUCTURE
AF
GVI
420
GENERAL VISUAL INSPECTION OF THE FAN EXIT FLOW PATH
SURFACES.
ACCESS: 415AL
425AL
783700-N1-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -78
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
792000-N1-1
792000-N2-1
792000-N3-1
792000-P1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 DISTRIBUTION - GENERAL
420
CLEAN PRESSURE OIL FILTER ELEMENT.
EN
410 DISTRIBUTION - GENERAL
420
DISCARD PRESSURE OIL FILTER ELEMENT.
EN
410 DISTRIBUTION - GENERAL
420
DISCARD SCAVENGE OIL FILTER ELEMENT.
EN
RST
I: 10000 FH
SOURCE
MRB 6
792214-100-801
MEN
M/H
APPLICABILITY
1
1
0.28 TRENT 7000
0.28
1
1
0.15 TRENT 7000
0.15
1
1
0.15 TRENT 7000
0.15
1
1
0.10 PW
0.10
*
*
0.10
0.10
1
1
0.50 PW
0.50
*
*
0.13
0.13
1
1
0.40 PW
0.40 POST SB PW 79-29
PRE SB PW 79-37
MRB REFERENCE:
79.20.00/01-RN
DIS
I: 20000 FH
MRB 6
DIS
I:
2500 FH
MRB 6
792216-960-801
MRB REFERENCE:
79.20.00/03-RN
413 ENGINE OIL SYSTEM DISTRIBUTION
EN
DET
423
INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES.
I:
800 FH
MRB 6
EN
DIS
792200-200-801
MRB REFERENCE:
72.34.00/01-PW
72.41.00/02-PW
72.54.00/01-PW
72.61.00/01-PW
79.20.00/01-PW
ACCESS: 417DL
427DL
410 OIL DISTRIBUTION
420
DISCARD ENGINE OIL FILTER ELEMENT.
792214-960-801
MRB REFERENCE:
79.20.00/02-RN
NOTE:
ETOPS RELEVANT
792000-P3-1
REFERENCE
I:
NOTE
MAN
792122-920-801
MAN
PW4G-100-1-96
NOTE:
- REFER TO MAN-PW4G-100-1-96 FOR INTERVAL
ACCESS: 415BL
425BL
792000-P5-1
416BR
426BR
417AL
427AL
418AR
428AR
410 OIL DISTRIBUTION
EN
DET
420
DETAILED INSPECTION OF NO.4 BEARING SCAVENGE TUBE
ASSEMBLY CLAMPS FOR BENT OR CRACKED TUBES AND CLAMP
MIGRATION
* * * * *
C O N T I N U E D
SYSTEMS, APU AND POWER PLANT : ENGINE OIL
I:
600 FH
CMP
VSB
VSB
PW4G-100-79-36
CMP REFERENCE:
72-2-0204-008
* * * * *
REV. DATE: JUL 01/21
SECTION:
2 -79
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
792000-P5-1
ZONE
* * * * *
C O N T I N U E
ACCESS: 415BL
425BL
N
792000-P6-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
416BR
426BR
417AL
427AL
410 ENGINE OIL SYSTEM DISTRIBUTION
420
DISCARD OIL PRESSURE FILTER.
SOURCE
REFERENCE
MEN
M/H
*
*
0.13
0.13
APPLICABILITY
* * * * *
418AR
428AR
EN
DIS
I:
2000 FH
MRB 7
MRB REFERENCE:
79.20.00/02-PW
1
1
TBD PW
TBD
410 OIL DISTRIBUTION
EN
420
REMOVE, CLEAN AND REINSTALL PRESSURE OIL FILTER
ELEMENT.
RST
I:
1600 FH
MRB 6
792243-100-801
1
1
0.30 TRENT 700
0.30
*
*
0.10
0.10
1
1
0.30 TRENT 700
0.30
*
*
0.10
0.10
1
1
0.25 TRENT 700
0.25 WITH EMCD NOT
INSTALLED
PRE SB RB 79-G229
*
*
0.02
0.02
NOTE:
ETOPS RELEVANT
792000-R1-1
MRB REFERENCE:
79.20.00/02-RR
NOTE:
ETOPS RELEVANT
ACCESS: 415AL
425AL
792000-R2-1
410 OIL DISTRIBUTION
EN
420
REMOVE, DISCARD AND REPLACE OIL SCAVENGE FILTER.
ACCESS: 415AL
425AL
792000-R3-1
416AR
426AR
DIS
I:
1600 FH
MRB 9
792245-920-801
MRB REFERENCE:
79.20.00/03-RR
416AR
426AR
410 OIL DISTRIBUTION
EN
DET
420
INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF
ABNORMAL DEPOSITS.
I:
130 FH
MRB 6
790000-200-805
MRB REFERENCE:
72.33.00/02-RR
72.33.40/01-RR
72.61.00/01-RR
79.20.00/01-RR
NOTE:
ETOPS RELEVANT
ACCESS: 416BR
426BR
SYSTEMS, APU AND POWER PLANT : ENGINE OIL
REV. DATE: JUL 01/21
SECTION:
2 -79
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
792100-G1-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
410 LUBRICATION
420
CHECK THE MASTER MAGNETIC CHIP DETECTOR FOR
PARTICLES.
EN
DET
I:
1000 FH
SOURCE
MRB 6
REFERENCE
792111-210-801
ACCESS: 414BL
424BL
410 LUBRICATION
420
DISCARD OIL SCAVENGE FILTER ELEMENT.
ACCESS: 415AL
425AL
793000-R3-1
EN
DIS
I:
24 MO
OR
10000 FH
MRB 6
MRB REFERENCE:
79.20.00/01-G6
EN
RST
I:
2500 FH
MRB 6,9
793000-R4-1
410 OIL INDICATING SYSTEM
420
DETAILED INSPECTION OF EMCD.
792246-910-801
MRB REFERENCE:
79.30.00/01-RR
ACCESS: 416BR
426BR
R
792143-920-801
416AR
426AR
410 OIL INDICATING SYSTEM
420
CLEANING AND FUNCTIONAL CHECK OF EMCD.
EN
DET
I:
130 FH
MRB 6
790000-200-822
MRB REFERENCE:
72.33.00/04-RR
72.33.40/02-RR
72.61.00/02-RR
79.30.00/02-RR
NOTE:
ETOPS RELEVANT
ACCESS: 416BR
426BR
* * * * *
E N D
SYSTEMS, APU AND POWER PLANT : ENGINE OIL
M/H
APPLICABILITY
1
1
0.05 GE
0.05
*
*
0.01
0.01
1
1
0.15 GE
0.15
*
*
0.10
0.10
1
1
0.25 TRENT 700
0.25 WITH EMCD ACTIVATED
POST SB RB 79-F524
*
*
0.02
0.02
1
1
0.25 TRENT 700
0.25 PRE 56713
IF EMCD INSTALLED
*
*
0.02
0.02
MRB REFERENCE:
72.20.00/03-G6
72.30.00/02-G6
72.50.00/03-G6
72.60.00/01-G6
79.20.00/02-G6
NOTE:
ETOPS RELEVANT
792110-G1-1
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-79
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
800000-P2-1
ZONE
413 ENGINE STARTING SYSTEM
423
CHANGE STARTER OIL.
ACCESS: 415BL
425BL
800000-P3-1
801100-N2-1
SVC
I:
600 FH
SOURCE
MRB 6
REFERENCE
121380-610-803
MRB REFERENCE:
80.00.00/02-PW
418AR
428AR
DET
I:
600 FH
MRB 6
801118-200-801
416AR
426AR
EN
416AR
426AR
410 PNEUMATIC STARTER
420
STARTER OIL CHANGE
SVC
M/H
APPLICABILITY
1
1
0.30 PW
0.30
*
*
0.13
0.13
1
1
0.10 PW
0.10
*
*
0.07
0.07
I:
1600 FH
MRB 6
121380-600-802
1
1
0.30 GE
0.30
*
*
0.20
0.20
1
1
0.05 GE
0.05
*
*
0.20
0.20
1
1
0.80 TRENT 7000
0.80
1
1
0.43 TRENT 7000
0.43
MRB REFERENCE:
80.00.00/01-G6
417AL
427AL
418AR
428AR
417AL
427AL
EN
DET
I:
1600 FH
MRB 6
801141-210-801
MRB REFERENCE:
80.00.00/04-G6
418AR
428AR
EN
SVC
410 PNEUMATIC STARTER
EN
DET
420
DETAILED INSPECTION OF STARTER MAGNETIC CHIP DETECTOR
SYSTEMS, APU AND POWER PLANT : ENGINE - STARTING
MEN
MRB REFERENCE:
80.00.00/03-PW
418AR
428AR
410 ENGINE STARTER
420
INSPECTION OF STARTER CHIP DETECTOR.
ACCESS: 415AL
425AL
801100-N1-1
417EL
427EL
410 ENGINE STARTER
420
STARTER OIL CHANGE.
ACCESS: 415AL
425AL
801100-G3-1
416BR
426BR
EN
413 ENGINE STARTING SYSTEM
EN
423
INSPECT STARTER CHIP DETECTOR FOR PARTICLES.
ACCESS: 416BR
426BR
801100-G1-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
I:
750 FH
MRB 6
121380-600-803
MRB REFERENCE:
80.11.00/01-RN
I:
750 FH
MRB 6
801100-220-801
MRB REFERENCE:
80.11.00/02-RN
REV. DATE: JUL 01/21
SECTION:
2-80
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
801100-R1-1
ZONE
410 PNEUMATIC STARTER AND VALVE SYSTEM
420
STARTER OIL REPLENISHMENT.
ACCESS: 415AL
425AL
801100-R2-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
EN
SVC
* * * * *
400 FH
MRB 6,9
REFERENCE
801141-600-803
MRB REFERENCE:
80.11.00/02-RR
416AR
426AR
410 PNEUMATIC STARTING
EN
SVC
420
STARTER OIL CHANGE AND INSPECTION OF STARTER CHIP
DETECTOR.
ACCESS: 415AL
425AL
I:
SOURCE
I:
800 FH
MRB 6,9
801141-600-801
SYSTEMS, APU AND POWER PLANT : ENGINE - STARTING
M/H
APPLICABILITY
1
1
0.05 TRENT 700
0.05
*
*
0.10
0.10
1
1
0.50 TRENT 700
0.50
*
*
0.10
0.10
MRB REFERENCE:
80.11.00/01-RR
416AR
426AR
E N D
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
2-80
PAGE 2
MAINTENANCE PLANNING DOCUMENT
3- STRU
CTUR
E
INTRODUCTION
1. GENERAL
The purpose of this section is to maintain the continuous airworthiness of the aircraft structure and to
control corrosion to Level 1 or better (refer to “CORROSION PREVENTION AND CONTROL PROGRAM
(CPCP)” for definition of Level 1 corrosion).
The Structure section contains FC-and FH-optimized requirements. Instructions are given in paragraph 11
of this section.
ISSUE: JUL 01/21
STRUCTURE
Page 1
MAINTENANCE PLANNING DOCUMENT
2. INSPECTION PHILOSOPHY
This section has been developed by considering the following sources of damage:
1. Metallics
(FD) Fatigue Damage
For FD, the damage initiation and subsequent damage growth is primarily dependant on the ground
air ground loading variation, which occurs once per flight. Therefore, flight cycles (FC) are used as the
unit for thresholds and repeat intervals. Some fatigue related SSI’s are also sensitive to flight duration.
For these SSI’s, a FH limit is stated in addition to the FC limit. The inspection is to be performed at
whichever limit is reached first.
The structure inspection tasks selected for fatigue are derived from damage tolerance evaluation
according to the criteria defined by FAR/JAR 25.571, Amendment 45. The FC and FH data is based
on a combination of calculation, full-scale fatigue test tear down results, and in-service experience
(where available).
(ED) Environmental Deterioration
Since deterioration caused by the environment (e.g. corrosion, stress corrosion) is mainly time
dependant, the maintenance requirements are based on calendar time (Years).
(AD) Accidental Damage
For deterioration caused by accidental damage, it is considered that major damage such as that
caused by bird impact, or ground handling equipment, will be detected by routine inspections. AD
consists of minor damage which could result in fatigue and/or corrosion damage, and which could
propagate undetected. In the analysis, the fatigue and environmental effects of the accidental damage
are considered. A dedicated AD task is not selected; the AD requirement is consolidated into either
the ED or the FD task, or both, according to the AD consequences. AD is therefore subject to
maintenance requirements expressed in FC (and FH) or calendar time or both.
2. Non-metallics
(AG) Ageing Deterioration
Deterioration caused by ageing considers loading conditions and environmental conditions. Inspection
intervals and thresholds are based on calendar time.
(AD) Accidental Damage
Deterioration caused by accidental damage is subject to inspection intervals based on calendar time.
The frequency of inspection is dependant on static strength reduction caused by the selected
damage, combined with the likelihood of the selected damage occurring more than once during the
selected interval.
As this kind of deterioration is random in nature, inspections shall be applied to all aircraft at each
repeat interval without threshold.
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3. INSPECTION LEVELS
According to the analysis procedure, for each Structural Significant Item (SSI), various inspection levels
have been considered with the aim of selecting the lowest inspection level compatible with the type of
damage and the expected damage growth. Therefore, one or more of the following inspection levels have
been selected for each SSI:
General Visual Inspection (GVI)
Detailed Inspection (DET)
Special Detailed Inspection (SDI)
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4. ZONAL SECTION COMPATIBILITY
When General Visual Inspection (GVI) level has been selected for a particular structure inspection task in
the Structure section of the MRBR, the inspection requirement is considered adequately covered by the
equivalent Zonal (ZIP) tasks which are referenced in the ZIP reference column. The MRB Report
Structure section GVI tasks which have a ZIP reference are therefore not listed as individual tasks in the
MPD.
GVI maintenance tasks which are not compatible with the Zonal section are stated in the MPD as
individual tasks. GVI SSI's which also require the addition of Temporary Protection Systems (TPS) will still
be indicated as individual tasks in the Structure section. The TPS application remains a Structure
requirement but the inspection part of the maintenance task may be covered by the Zonal Inspection.
Refer to paragraph 4 of the introduction of the A330 MRBR Structure section for additional details.
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5. SAMPLING PROGRAM
A. INTRODUCTION
The Sampling Program is designed to detect systematic deterioration caused by the environment on
a group of aircraft selected from those which have the highest age within a considered fleet.
The Sampling Program is applicable to Environmental Deterioration (ED) SSIs, where the
deterioration, should it occur, is considered as being progressive with age. SSIs which are
susceptible to Accidental Damage (AD) are not considered for the Sampling Program .
Structure inspections fall into the following 2 categories:
100%
Corrosion tasks where accidental damage is likely or where in-service experience indicates that
damage is likely are not selected for sampling. These tasks have a 100% threshold only. e.g.
534127-01-1.
100% + SAMPLING
Corrosion tasks where in-service experience indicates that damage is not likely are selected for
sampling. These tasks have a sampling threshold. All aircraft not inspected as sampling aircraft
must be inspected at the 100% threshold (24 years). e.g. 545126-02-1.
Based on the results of Sampling Program inspections:
–
–
In case of findings, each operator should take appropriate corrective actions, such as change of
program concept to 100%, decrease of interval, application of TPS etc.
In case of no findings, the current inspection program continues to apply.
B. SELECTION OF AIRCRAFT FOR SAMPLING PROGRAM
For each operator, the Sampling Program inspections are to be performed on the oldest 1/5 of the
operator's A330 aircraft.
The oldest aircraft are defined as the aircraft with the highest age in years since their initial
manufacturer's delivery date.
From MRBR Rev 17, the A330 sampling fleet is no longer determined by WV Group. The
determination is done between PAX (A330-200/-300/-800/-900) or Freighter Aircraft (A330- 200F).
Operators with both PAX and Freighter aircraft should select the oldest 1/5 PAX aircraft and the
oldest 1/5 of A330-200F.
For operators with more than one aircraft type in their fleet, e.g A330 and A340, the Sampling
Program aircraft should be determined per aircraft type, e.g. 1/5 of the oldest A330 aircraft + 1/5 of
the oldest A340 aircraft.
If the 1/5 sample of the operators aircraft is not a whole number of aircraft, the number is to be
decreased to the next lowest whole number.
A minimum of one aircraft per operator must be selected for the Sampling Program. The maximum
number of aircraft to be sampled per operator is 5 aircraft per aircraft type even if the total fleet size
would lead to a higher number applying the 20% rule.
NOTE: Operators operating the same aircraft type in similar operational conditions and having
established common rules acceptable to each operators' Airworthiness Authority may
combine their fleets to form one fleet for the Sampling Program.
A minimum of one aircraft must be selected from each operator in the group, if not already selected
by the above rule.
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Any aircraft in a fleet is protected by the respective sample aircraft of this operator’s fleet. If a “nonsampling” aircraft would be integrated into a new operator’s fleet it could become a sampling
aircraft. However, no retroactive maintenance is required i.e. all inspections are to be performed at
their next due.
Example: An aircraft which was not a sample A/C is 7 years old has been acquired by another
operator. All inspections with an interval of 6 YE would be due at the next 6 YE check; which is 12 YE
after entering service.
Any significant changes to an operator's fleet will require a review of the Sampling Program aircraft.
This includes buying and/or selling aircraft and retiring aircraft from the fleet. Operators may contact
Airbus for advice in the selection of the Sampling Program aircraft.
Sampling tasks only need to be performed on aircraft selected for Sampling. Therefore only Sampling
tasks applicable to the modification status of the selected Sampling aircraft need to be performed.
This means that some sampling tasks may not be performed on an individual operator’s fleet. The
fleet of the operator is protected by the tasks performed in the world fleet by operators whose Sample
aircraft are of the relevant modification status. Any significant findings will be reported and acted
upon.
C. ARRANGEMENT OF INSPECTIONS
For the selected sampling A/C, the inspections commence at the Sample or 100% Threshold
(whichever occurs first) and continue at each subsequent repeat interval (Sample Interval or 100%
Interval, whichever occurs first).
NOTE: Different source document requirements (e.g. MRBR and ALI) consolidated in one MPD
task may lead to a task which has a 100% Threshold/Interval which is lower than the
Sample Threshold/Interval. In this case the more conservative 100% requirement must be
followed.
To ensure that operators do not miss 100% requirements on sampling aircraft, the 100%
values have been added to the Sampling requirement in these cases.
NOTE: For the Threshold/Interval selection of the sampling A/C it is mandatory to follow the
sampling logic as shown in below paragraph “SAMPLING PROGRAM ILLUSTRATIONS”.
NOTE: For all aircraft not selected for sampling only the 100% Threshold/Interval must be taken
into account (refer to the suitable example on the following pages).
D. SAMPLING PROGRAM ILLUSTRATIONS
A chart presenting the way to deal with the sample/100% threshold and interval is shown below.
The Sampling Program aircraft should first be selected before the subsequent planning of the SSI
details.
NOTE: The example Sample Program Illustration are no longer listed in the MPD. Please refer
directly to the Section D Introduction of the MRBR for accessing them.
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6. CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)
A. INTRODUCTION
The Structure section includes requirements to control corrosion to Level 1 or better on all structural
details, elements or assemblies whose failure could affect the structural integrity necessary for the
safety of the aircraft
All Corrosion Prevention and Control Program (CPCP) requirements are indicated by the code
'CPCP' in the “SOURCE” column.
Some Calendar-time tasks are also covered by the Sampling Program, i.e. they have a Sample
Threshold/Interval. For these tasks, the 100% Threshold is the time at which the task becomes a
CPCP task.
B. CORROSION LEVEL DEFINITIONS
The severity of the corrosion damage is categorized into three 'Levels' as follows:
Level 1 Corrosion
Corrosion damage that does not require structural reinforcement or replacement.
or
Corrosion occurring between successive inspections exceeds allowable limit but is local and can
be attributed to an event not typical of operator usage of other aircraft in the same fleet (e.g.
Mercury spill).
Level 2 Corrosion
Corrosion occurring between successive inspections that requires a single rework/blend out
which exceeds allowable limits as defined by the manufacturer (SRM, SB, etc.), requiring a
repair/reinforcement or complete or partial replacement of applicable structure.
Level 3 Corrosion
Corrosion found during first or subsequent inspection(s), which is determined (normally by the
operator) to be an urgent airworthiness concern requiring expeditious action.
C. CPCP RULES
The effectiveness of the CPCP is determined by following the General Rules applicable to the
Structure section and by following the rules listed below:
Level 1 Corrosion Findings
Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat
inspections on particular aircraft operated in similar conditions, then the existing program is
considered effective for the concerned area, and no change to the program is necessary.
Specifically for Landing Gear corrosion findings at Overhaul, Level 1 corrosion is interpreted to
include cases of light corrosion that is within allowable limits but requires structural replacement,
since a repair has not been defined or is not economically viable.
Level 2 Corrosion Findings
Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections, then
the existing program is not effective for the concerned area of the particular fleet.
In order to control corrosion to Level 1 or better, consideration should be given to one or more of the
following corrective actions:
–
–
–
–
Decreasing the inspection threshold/interval
Considering a higher inspection level
Re considering the Program Concept
Application/More frequent application of Temporary Protection System
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–
–
Embodiment of preventive modifications, where applicable
Installation of parts with improved protection standard, where applicable.
In this way, the program is self regulating and will adjust itself to the optimum program.
Level 3 Corrosion Findings
Should inspections reveal that corrosion is Level 3 in a given area, then the existing program is not
effective for the concerned area.
In addition to the considerations given for Level 2 corrosion, an action plan calling for a one time
inspection of the concerned area should be expeditiously agreed with the local Aviation Authority and
carried out on all aircraft of a similar age or older.
Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all
details of findings are to be promptly reported for detailed evaluation and the assistance required
clearly expressed.
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7. FATIGUE MONITORING PROGRAM
A. GENERAL
The Fatigue Monitoring Program (FMP) is defined to indicate unexpected early occurrence of fatigue
related deterioration on metallic structure.
The FMP tasks are established for inspection in advance of the calculated 100% Fatigue Damage
(ALS Part 2) threshold inspection. The FMP tasks are expressed in calendar time to enable operators
to plan task accomplishment within existing planned heavy maintenance checks (i.e. at 6 years
multiples or equivalent operator’s heavy maintenance event interval).
The process to establish the FMP has been discussed and accepted by the EASA certification and
aircraft maintenance branches.
The FMP is part of the Airbus Ageing Airplane monitoring process. FMP tasks selection, task reviews
and adjustments of the global FMP are addressed in the Structure Task Group (STG) meetings.
The FMP allows operators to adjust or remove a FMP task from its Operator’s Maintenance Program
(OMP). This is based on confirmed nil findings/non-significant findings on a certain proportion of the
operator’s fleet. This could be done through Operator’s Reliability Program.
FMP requirements are identified as “MRB FMP” in the MPD source column.
B. FMP Applicability
The FMP is a configuration based monitoring programme.
All aircraft within the operator’s fleet in the structural configuration identified in the FMP task
applicability are subject of the FMP requirement.
C. FMP Requirements Fulfilment
The aim of a FMP requirement is fulfilled in case at least 10 aircraft within one operator’s fleet (or
from different operators belonging to the same airlines group, managed by the same maintenance
organization and with identical FMP task content on all OMP) have accomplished the FMP task at the
inspection threshold and reported (see paragraph: FMP Tasks Reporting).
Once FMP requirement is fulfilled, the FMP task may be adjusted or deleted from the Operator’s
Maintenance Program (OMP), depending on the FMP requirement type (see paragraph: FMP Task
Type).
Credit cannot be taken from previous accomplishment of FMP tasks by other operator unless
managed under the same maintenance organization.
Credit can be taken from previous accomplishment of former related Fatigue Sampling tasks as long
they were managed by the same maintenance organization at any of the previous heavy
maintenance checks of the aircraft.
Alternatively operators may accomplish FMP tasks on all aircraft subject of FMP task applicability in
their fleet and update their OMP based on the global adjustment of the FMP inspection task. This is
performed during STG meetings and provided in the MRBR Appendix 14 (FMP).
D. FMP Tasks Type
There are two types of FMP tasks depending on whether there is an existing associated 100%
fatigue requirement (ALS Part 2) or not:
–
–
FMP tasks without associated ALS Part 2 (NOTE A FMP tasks)
FMP tasks with associated ALS Part 2 (NOTE B FMP tasks)
(1) FMP tasks without associated ALS Part 2 (NOTE A FMP tasks)
FMP tasks without an associated ALS Part 2 task are designated as NOTE A FMP tasks.
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NOTE A FMP tasks provide a threshold (in Calendar Time) and a repeat interval at 6 YE.
NOTE A FMP tasks are subject for threshold adjustment in OMPbased on its inspection results:
–
–
–
–
In case a minimum of 10 aircraft have been inspected at the NOTE A FMP task threshold
Airbus should be informed about the inspection results (see paragraph: FMP tasks Reporting).
Airbus will acknowledge receipt of the inspection result via Tech Request.
The operator may increase the NOTE A FMP task threshold by 6 YE (or the equivalent
operator’s heavy maintenance interval) in its OMP.
The adjusted NOTE A FMP task threshold is applicable for the individual operator even in
case the fleet is renewed.
Example:
An operator accomplished a NOTE A FMP inspection on 10 MSN with NIL findings, reported
the inspection results to Airbus and increased the NOTE A FMP task threshold from 18 YE to
24 YE. At an aircraft age of 22 YE the operator renews its fleet and adds new aircraft with the
same configuration as the one subject for the NOTE A FMP task. The NOTE A FMP task
threshold remains at 24 YE in the OMP, so the operator can take benefit from previously
accomplished inspections.
Operators with a fleet of less than 10 aircraft as per NOTE A FMP task applicability may also
report nil-finding/non-significant findings task accomplishments to Airbus. This data will be used
to support global NOTE A FMP tasks adjustment /deletion during periodic STG meetings.
(2) FMP tasks with associated ALS Part 2 (NOTE B FMP tasks)
FMP tasks with an associated ALS Part 2 task are designated as NOTE B FMP tasks.
NOTE B FMP tasks provide a threshold (in Calendar Time) to be accomplished in advance of the
associated 100% fatigue requirement (ALS Part 2).
NOTE B FMP tasks are subject for deletion in OMP based on its inspection results:
–
–
–
In case a minimum of 10 aircraft have been inspected at the NOTE B FMP task threshold
Airbus should be informed about the inspection results (see paragraph: FMP tasks Reporting).
Airbus will acknowledge receipt of the inspection result via Tech Request.
The operator may delete the NOTE B FMP task from its OMP.
Example:
An operator has more than 10 A/C in line with the applicability of an FMP task provided. After
accomplishment of 10 inspections in advance of the associated ALS Part 2 FC/FH inspection
requirement the results should be reported to Airbus. Airbus will acknowledge receipt of the
report and the operator can terminate this NOTE B FMP task from its maintenance program.
Operators with a fleet of less than 10 aircraft as per NOTE B FMP task applicability may also
report nil-finding/non-significant findings task accomplishments to Airbus. This data will be used
to support global NOTE B FMP tasks evolution/deletion in the FMP task reviews during periodic
STG meetings.
Rules to apply for a NOTE B FMP task and its associated 100% fatigue requirement (ALS Part 2):
1.
In case the NOTE B FMP task and its associated 100% fatigue requirement (ALS Part 2) have
the same inspection procedure, it is up to operator’s choice to decide whether to count the NOTE
B FMP task accomplishment as the ALS Part 2 Threshold inspection.
Above statement is not applicable in case the NOTE B FMP task and its associated 100% fatigue
requirement (ALS Part 2) have a different inspection procedure.
2.
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If an airplane reaches the FC or FH of the associated 100% fatigue requirement (ALS Part 2)
threshold in advance of the NOTE B FMP task threshold then the 100% fatigue requirement has
to be followed (ALS threshold FC or FH, whichever occurs first) and the NOTE B FMP task
applicability may be updated to exclude the very aircraft from the OMP.
E. FMP Tasks Reporting
FMP tasks are subject for review based on operator’s feedback of FMP tasks accomplishment.
(Refer to MRBR Appendix 6 for reporting system).
Reporting is key for FMP global adjustment and efficiency.
Minimum data that the report should contain:
–
–
–
–
–
MSN
Inspection date
FC and FH
Inspection result (Findings/nil findings)
In case of findings: Damage description
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8. GENERAL RULES APPLICABLE TO THE STRUCTURE SECTION
1. The Maintenance tasks are to be carried out 'at or before' the limits stated for Sample
Threshold/Interval and 100% Threshold/Interval. Where a task has more than one limit, e.g. one in FC
and another in calendar time, the limit expiring first shall apply.
2. The Threshold is the time at which the maintenance requirement is first due.
• For FC or FH tasks without MOD applicability, the 100% thresholds are counted from first flight.
• For FC or FH tasks with MOD applicability, the 100% thresholds are counted from point of MOD
embodiment, unless otherwise stated.
• For tasks in Years, the sample thresholds and 100% thresholds are counted from the date of initial
delivery from the manufacturer, unless otherwise stated (NOTE 8).
3. For repeat maintenance tasks, the interval starts at the time of the last maintenance tasks performed.
4. Thresholds and intervals quoted in calendar time in this section include aircraft time in and out of
service. In other words, operators will not, in general, be allowed to take credit for time out of service
or storage periods to extend corrosion inspection intervals.
5. It is assumed that the structure to be inspected is in a state of cleanliness which allows a satisfactory
inspection to be carried out at the required inspection level.
Where existing Temporary Protection System (TPS) permits unobscured assessment of the condition
of the structure, TPS may remain in place for the inspection.
6. If damage is found or suspected (such as bulging skin) then the full extent of any damage must be
clearly identified using appropriate inspection techniques and/or disassembly when necessary. This
may require additional access to that stated for the maintenance task.
All damage is to be evaluated and repaired in accordance with documentation acceptable to the
relevant Airworthiness Authority.
7. If inspections indicate evidence of deterioration, appropriate further actions must be taken to prevent
similar deterioration occurring in the operators fleet.
For corrosion findings refer to Corrosion Prevention and Control Program in this section.
8. The following applies to Temporary Protection System (TPS) application:
Prior to any application of TPS, perform an inspection of the area at the inspection level for the task
quoted in calendar time.
Prior to re fitting/re connecting/re installing parts removed to gain access to the inspection area, TPS
is to be applied to each SSI, as quoted in the TPS column of this Structure section, at least as
frequently as the calendar time thresholds and intervals of the respective SSI. For SSI's where the FC
or FH limit is reached before the calendar time limit, consideration should be given to application of
TPS at the FC or FH limit
The Type of TPS to be applied is provided in the TPS column of the Structure section.
When TPS is only applied to a selected area, details are provided as a note in the Description
column.
Sampling Program tasks do not have TPS selected in the Structure section. If an operator chooses to
apply TPS to a particular SSI for aircraft inspected in accordance with the Sampling Program, these
aircraft are no longer representative of the non-sampled aircraft. In this case, TPS must be applied to
all aircraft in this SSI area, including the aircraft not selected for sampling. This task then effectively
becomes 100% for those specific aircraft.
CAUTION:
Do not apply TPS on oxygen systems, control cables, pulleys, Teflon bearings and lubricated
surfaces.
Drain valves and all open orifices are to be protected from ingress prior to temporary protection being
applied.
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9. The access column may contain one of the following instructions concerning insulation blankets:
Insulation = Insulation to be removed from the inspection area.
Note 1 = Insulation to be displaced as required to complete the required maintenance task.
10. Ensure wet insulation blankets are dried prior to reinstallation, or replaced with new.
11. Ensure that all drain holes and drainage paths are clear from obstruction.
12. The condition of the paint system should be verified during the inspections. Re protection should be
applied where necessary.
13. The requirements stated in years were determined for an aircraft operated in a moderate humidity
environment and not subjected to corrosive products.
Any operators who routinely operate in humid or marine environments and/or carry corrosive cargo
such as seafood, may find that the calendar time maintenance tasks stated in this MPD are not
sufficient to control corrosion to Level 1 or better. Operators in this category should take appropriate
further actions.
14. Operators shall report inspection results related to SSI's to the manufacturer in accordance with the
Maintenance Task Reporting System. Refer to the General Introduction paragraph 15.
Note: This reporting requirement does not take precedence over existing national requirements for
occurrence reporting.
15. Based on reports made through the Maintenance Task Reporting System, Airbus will:
– Inform all the operators of the significant discrepancies discovered on the A330 fleet.
– Make the appropriate recommendations.
16. “Touch and Go" Cycles can be neglected if they are less than 5% of the total number of Flight Cycles
up to threshold inspection or between two consecutive inspections.
Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold
inspection or between two consecutive inspections.
17. Additional information concerning SSI inspections is provided in the following Airbus supporting
publications:
• Maintenance Review Board Report (MRBR)
• Airworthiness Limitation Items (ALI)
• Aircraft Maintenance Manual (AMM)
• Non-Destructive Testing Manual (NTM)
• Structural Repair Manual (SRM)
18. In the event that the first task is accomplished very early, such that the period (Calendar time, FC,
FH) between initial task accomplishment and the threshold is greater than the interval, the next task
can be performed at the threshold (rather than the repeat interval).
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9. SECTION NOTES
NOTE 1 to 6
and 8 to 10:
The Content of MRBR Section D Notes is given as full text in the corresponding
MPD task.
NOTE 7:
Minimum major improvements for cabin floor structure. Refer to SIL 53-091 / ISI
53.00.00106 for details.
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10. WEIGHT VARIANT APPLICABILITY
The A330 aircraft have different fatigue inspection requirements for the various Weight Variants (WV) of
each aircraft. The Weight variant represents the delivery standard of each aircraft.
The applicable Weight Variant for each individual aircraft can be found in Table 1 of the “Aircraft
Allocation List” in the Structure Repair Manual (SRM) Intro.
Table 2 of the SRM “Aircraft Allocation List” gives additional data for aircraft which have the weight
Variant status amended due to modifications or Service Bulletin embodiment.
To minimize the number of individual inspection requirements, the Weight Variant requirements have
been grouped where they are similar. The group number is stated in the Structure section
“APPLICABILITY” column. Refer to the details below:
WV Group
A/C Series
Weight Variants
GROUP 32A
A330-200
020, 021, 022, 023, 024, 025, 026, 027
GROUP 32E
A330-200
050, 051, 052, 053, 054, 055, 056, 057, 058, 059, 060, 061,
062, 080, 081, 082, 083
GROUP 32F
A330-200F
000, 001, 002
GROUP 33A
A330-300
000, 001, 002, 003, 004
GROUP 33B
A330-300
010, 011, 012, 013, 014
GROUP 33C
A330-300
020, 024, 025, 026, 027
GROUP 33D
A330-300
022
GROUP 33E
A330–300
030, 031, 032, 033, 034, 035, 039, 050, 051, 052, 053, 054,
055, 056, 057, 058, 080, 081, 082, 083
GROUP 38E
A330–800
800, 801, 802
GROUP 39E
A330–900
900, 901, 902
INTERPRETATION
GROUP 32A
3 : Aircraft Type 3 for “A330”
2 : Model 2 for “-200”
A : 1st Weight Variants Group identified in the specific certified Type “A330” / Model “-200“ which
is comprised of 020, 021, 022, 023, 024, 025, 026, 027.
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11. AIRCRAFT UTILIZATION LIMITS / LIMIT OF VALIDITY (LOV)
A330 aircraft are certified against utilisation limits expressed in FC and FH.
The Limit Of Validity (LOV) and Maintenance Program Publication Trigger are provided in the introduction
of the A330 ALS Part 2 Document.
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12. FC- AND FH-OPTIMIZED DATA SETS
A. BACKGROUND
Airbus periodically conducts Structural Fleet Surveys to monitor Fleet usage. The 2008 Fleet Survey
revealed a larger range of A330 fleet FC and FH utilisation than previously recorded. Existing
Thresholds and Intervals of the range-sensitive fatigue tasks therefore required revising to ensure the
coverage of the A330 aircraft fleet.
An initial assessment indicated that this would result in very significant Threshold/Interval reductions
if applied to the existing method of calculation (single set of fatigue figures). This would have
penalised both short and long range A330 operators. In order to limit the impact, Airbus produced 2
sets of fatigue data for all Thresholds/Intervals of fatigue inspection tasks sensitive to range. These 2
sets of data are produced based on a trade-off between Flight Cycles (FC) and Flight Hours (FH).
This allows optimisation of the Maintenance Program according to the actual aircraft operation. This
data was first published in MRBR rev 14 and ALI doc rev 18 (ALS Part 2).
B. USE OF FC- AND FH-OPTIMIZED DATA
Both sets of data ensure the continuous airworthiness of the aircraft. Both sets of data are approved
for use on any A330 aircraft without restriction regarding the utilisation.
Operators can monitor their aircraft utilisation and optimize requirements accordingly. For a given
task, operators can use either set of FC or FH optimized data, as long as the pair of FC and FH
values from the same optimized data are selected.
Example:
Threshold/Interval:
FH and FC values from FH-optimized data
or
FH and FC values from FC-optimized data
Either set of data can be selected by any operator. However it may not be optimum.
For example, an operator with high annual FH utilisation will have a more optimum planning when
using the FH-optimized fatigue data. However, the operator could use the FC-optimized data and still
have an approved but non-optimized program. This is because the operator would be penalised by
the shorter FH limits of the FC-optimized program and would do the tasks earlier (threshold) or more
frequently (interval).
Consequently, the operator can select whichever set of figures is most appropriate for a particular
MSN, providing that the pair of FC and FH values are selected from the same set of data. In other
words:
–
The FC limit of the FC-optimized set can be selected, providing that the associated FH limit is also
selected (not exceeded).
OR
–
The FH limit of the FH-optimized set can be selected, providing that the associated FC limit is also
selected (not exceeded).
If the above rules are followed, both sets of data ensure the airworthiness of the aircraft.
The selection between the FC- and the FH-optimized sets can be done by the operator without any
restriction providing that the FC limit and the FH limit from the same set are considered (not
exceeded).
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MAINTENANCE PLANNING DOCUMENT
The limits for one task (FC and FH) must be taken from the same set of data.
C. OPTIMISATION OF PLANNING ACCORDING TO FC OR FH UTILISATION
Paragraph 11.2 states that operators can use either FC- or FH-optimized data to develop a
maintenance program and that both sets of data ensure the airworthiness of the aircraft. For planning
purposes, further optimisation could be performed if desired. Any operator can choose to have a
simple planning scenario by selecting one set of data (FH or FC), or can choose a more optimised
planning scenario, depending on utilisation. Some examples are given below:
•
Select the most appropriate data set for their fleet, either FC- or FH-optimized.
E.g. select FC- or FH-optimized set for the entire fleet.
OR
•
Select the most appropriate set by sub fleet or MSN within their fleet, FC-optimized for aircraft
with high average FC utilisation and FH-optimized for aircraft with high average FH utilisation.
E.g.: Select FC- or FH-optimized set according to sub-fleet or individual MSN utilisation.
OR
•
For a given task: Select the optimum set per MSN according to individual MSN utilisation. The
optimum planning for some aircraft will involve selecting a mixture of FC-or FH-optimized tasks on
a task-by-task basis. The full task must however be taken, i.e. pair of FC and FH values. From
either FC- or FH-optimized set.
E.g.: selecting tasks (pair of FC and FH values) from FC- or FH-optimized set on task-by-task
basis.
Refer to the following table which summarises the pros and cons of the 3 main planning scenarios:
•
•
•
METHOD
PROS AND CONS
SIMPLE
METHOD
Select 1 set
of data for
fleet
FC- or FHoptimized
According
to main
fleet
utilisation
Easy to plan
No flexibility for
mixed A/C
utilisation
Potential earlier
thresholds/
intervals for some
A/C
SEMIComplex to plan
OPTIMIZED
Some flexibility for
METHOD
mixed A/C
utilisation
ISSUE: JUL 01/21
STRUCTURE
Page 19
MAINTENANCE PLANNING DOCUMENT
•
•
•
•
•
•
Select 1 set
of data for
each subfleet or
MSN
FC- or FHoptimized
According
to utilisation
of each
sub-fleet or
MSN
Potential earlier
thressholds/
intervals for some
tasks & A/C
FULLYOPTIMIZED
METHOD
Select
optimum
tasks per
MSN
FC- or FHoptimized
According
to optimum
requirement
for task
Very complex to
plan
Full flexibility for all
A/C utilisations
Optimum
thresholds/intervals
for all tasks & A/C
Any of the above approaches is acceptable and all ensure the airworthiness of the aircraft. Operators
can therefore choose between a simple and a more optimized planning method.
ISSUE: JUL 01/21
STRUCTURE
Page 20
MAINTENANCE PLANNING DOCUMENT
TASK NUMBER
321101-01-1
321102-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG MAIN FITTING EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH
FLANGES.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG SLIDING PISTON EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY MAIN FITTING AND
BUSH FLANGES.
T:
6 YE
I:
6 YE
SOURCE
MRB CPCP
REFERENCE
321100-210-805
MRB REFERENCE:
321101-01-1
MRB CPCP
321100-210-806
MRB REFERENCE:
321102-01-1
PREP.: AIRCRAFT JACKING;
321104-02-1
321105-01-1
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG BOGIE BEAM, BOGIE BEAM
PIVOT PIN, BRAKE RODS AND BRAKE ROD PINS EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, BUSH
FLANGES AND STONE CHIP PROTECTIVE SEALANT.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG PITCH TRIMMER EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH
FLANGES.
T:
6 YE
I:
6 YE
MRB CPCP
321100-220-821
* * * * *
STRUCTURE : LANDING GEAR
C O N T I N U E D
1
1
0.20 ALL
0.20
1
1
0.25 ALL
0.25
*
2.50
1
1
0.50 ALL
0.50
MRB CPCP
321100-210-808
1
1
0.20 ALL
0.20
T:
6 YE
I:
6 YE
APPLICABILITY
MRB REFERENCE:
321105-01-1
*
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG UPPER & LOWER SIDE STAY,
UPPER PIN, LOWER PIN, CENTER PIN, UPPER CARDAN PIN &
NUT, LOWER CARDAN PIN & NUT, UPPER & LOWER SIDE STAY
SPRING BRACKETS, PIVOT LINK BRACKET, PIVOT LINK,
CONNECTING LINK, UPPER & LOWER SPRING BRACKET BOLTS,
PIVOT LINK BRACKET BOLTS, PIVOT LINK CENTER PIN, LOCK
LINK/SIDE STAY PIN, CONNECTING LINK/LOCK LINK/UPPER
SPRING PIN, CONNECTING LINK/PIVOT LINK PIN, LOWER
SPRING/PIVOT LINK PIN, CARDAN LINK, CARDAN LINK PIN,
LOCK LINK CENTER PIN & LOCK LINK UPPER PIN EXTERNAL
M/H
MRB REFERENCE:
321104-02-1
PREP.: MLG PITCH TRIMMER EXTENDED;
321106-02-1
MEN
MRB CPCP
321100-220-822
MRB REFERENCE:
321106-02-1
1
1
TBD
0.30 ALL
0.30
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-32
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
321106-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, BUSH
FLANGES AND FITTINGS.
R
N
321107-02-1
321107-02-2
321109-02-1
321110-02-1
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG UPPER & LOWER LOCK LINKS
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG UPPER & LOWER LOCK LINKS
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
T:
12 YE
I:
12 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG UPPER & LOWER TORQUE
LINKS, UPPER PIN, LOWER PIN, APEX PIN & APEX PIN NUT
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG UPPER ARTICULATION LINK
T:
6 YE
I:
6 YE
* * * * *
STRUCTURE : LANDING GEAR
C O N T I N U E D
MRB CPCP
321100-220-823
1
1
0.15 A330-200
0.15 PRE 54500
OR
A330-300
PRE 54500
OR
A330-800
PRE 54500
OR
A330-900
PRE 54500
1
1
0.15 A330-200
0.15 POST 54500
OR
A330-300
POST 54500
OR
A330-800
POST 54500
OR
A330-900
POST 54500
OR
A330-200F
1
1
0.20 ALL
0.20
1
1
0.10 A330-200
0.10 PRE 54500
OR
MRB REFERENCE:
321107-01-2
MRB
321100-220-823
MRB REFERENCE:
321107-01-3
MRB CPCP
321100-220-824
MRB REFERENCE:
321109-02-1
MRB CPCP
321100-220-825
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -32
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
321110-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
R
321125-03-1
MEN
321110-02-1
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG LOCK STAY/UNLOCK ACTUATOR
& ATTACHMENT PINS EXTERNAL SURFACES, EXCEPT WHERE
COVERED BY DRESSINGS AND BUSH FLANGES.
T:
6 YE
I:
6 YE
570 MAIN GEAR
AF
DET
670
DETAILED INSPECTION OF ECCENTRIC EARTHING PIN AND
EARTHING PIN
T:
10 YE
I:
10 YE
MRB CPCP
321100-220-827
1
1
0.15 ALL
0.15
1
1
0.05 A330-200
0.05 OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208040
OR
0.17 A330-900
PRE 208040
MRB REFERENCE:
321124-02-1
MRB CPCP
321100-220-845
MRB REFERENCE:
321125-03-1
PREP.: PINS AND NUT REMOVED;
321142-01-1
321146-01-1
*
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG RETRACTION LINK,
ADJUSTABLE LINK, BELLCRANK LINK, FORWARD PINTLE PIN,
FORWARD PINTLE PIN LOCK BOLT & PINS SM2, SM7, W, W1,
W2 & P EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS, FITTINGS AND BUSH FLANGES.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG RETRACTION ACTUATOR
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
T:
6 YE
I:
6 YE
570 MAIN GEAR
AF
DET
670
DETAILED INSPECTION OF MLG AFT PINTLE PIN, AFT PINTLE
T:
6 YE
I:
6 YE
* * * * *
STRUCTURE : LANDING GEAR
APPLICABILITY
A330-300
PRE 54500
NOTE:
- TO BE CARRIED OUT IN CONJUNCTION WITH SCHEDULED MLG
REMOVAL.
321136-01-1
M/H
* * * * *
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
321124-02-1
REFERENCE
C O N T I N U E D
MRB CPCP
321100-220-828
1
1
0.30 ALL
0.30
1
1
0.10 ALL
0.10
1
1
0.10 ALL
0.10
MRB REFERENCE:
321136-01-1
MRB CPCP
321100-220-829
MRB REFERENCE:
321142-01-1
MRB CPCP
321100-220-830
MRB REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -32
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
321146-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
N
321193-02-1
MEN
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF MLG LOWER ARTICULATING LINK &
PINS SL1, SL2, SL3, SL4 & SL5 EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH
FLANGES.
T:
6 YE
I:
6 YE
731 MAIN GEAR
AF
DET
741
DETAILED INSPECTION OF SHORTENING MECHANISM ECCENTRIC
EARTHING PIN AND SHORTENING MECHANISM EARTHING PIN
T:
12 YE
I:
12 YE
MRB CPCP
321100-220-831
1
1
322102-02-1
711 NOSE GEAR
DET
T:
6 YE
DETAILED INSPECTION OF NLG MAIN FITTING, TURNING
SLEEVE, UPPER FLANGE, LOWER FLANGE, LEVER, MAIN
FITTING HINGE PINS, UPPER & LOWER FLANGE ATTACHMENT
PINS AND STEERING ACTUATOR PISTON ROD ATTACHMENT PINS
EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS,
FITTINGS AND BUSH FLANGES.
I:
6 YE
T:
6 YE
I:
6 YE
711 NOSE GEAR
AF
AF
DETAILED INSPECTION OF NLG SLIDING TUBE, EXTERNAL
SURFACE.
DET
MRB
321100-220-847
1
1
MRB REFERENCE:
321193-02-1
MRB CPCP
322100-220-813
TBD A330-800
TBD POST 208040
OR
A330-900
POST 208040
*
0.17
1
0.40 ALL
1
0.30 ALL
*
2.50
MRB REFERENCE:
322101-02-1
MRB CPCP
322100-220-814
MRB REFERENCE:
322102-02-1
PREP.: AIRCRAFT JACKING;
SLIDING TUBE FULLY EXTENDED;
STRUCTURE : LANDING GEAR
0.10 ALL
0.10
MRB REFERENCE:
321148-01-1
PREP.: PINS AND NUT REMOVED;
R
APPLICABILITY
321146-01-1
NOTE:
TASK TO BE PERFORMED AT THE OPPORTUNITY OF LDG
REMOVAL.
322101-02-1
M/H
* * * * *
NUT, SHORTENING MECHANISM ECCENTRIC EARTHING PIN &
SHORTENING MECHANISM EARTHING PIN EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY MAIN FITTING AND PINTLE
BEARING.
321148-01-1
REFERENCE
REV. DATE: JUL 01/21
SECTION:
3-32
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
322103-02-1
322104-02-1
322105-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
711 NOSE GEAR
AF
DET
T:
6 YE
DETAILED INSPECTION OF NLG UPPER & LOWER TORQUE LINKS
AND TORQUE LINK UPPER, LOWER & APEX PINS, EXTERNAL
SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS
AND BUSH FLANGES.
I:
6 YE
123 NOSE GEAR
AF
DET
711
DETAILED INSPECTION OF NLG DRAG STAY UPPER ARM, DRAG
STAY UPPER PIN, CENTER PINS & PINTLE PIN EXTERNAL
SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS
AND BUSH FLANGES.
T:
6 YE
I:
6 YE
711 NOSE GEAR
T:
6 YE
I:
6 YE
DET
T:
6 YE
DETAILED INSPECTION OF NLG UPPER & LOWER LOCK LINKS,
LOCK LINK CENTER PIN AND LOCK LINK UPPER ARM TO MAIN
FITTING PIN EXTERNAL SURFACE, EXCEPT WHERE COVERED BY
DRESSINGS, FITTINGS AND BUSH FLANGES.
I:
6 YE
123 NOSE GEAR
AF
DET
711
DETAILED INSPECTION OF NLG RETRACTION ACTUATOR AND
ATTACHMENT PINS EXTERNAL SURFACE, EXCEPT WHERE
COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES.
T:
6 YE
I:
6 YE
123 NOSE GEAR
T:
10 YE
I:
10 YE
AF
DET
DETAILED INSPECTION OF NLG DRAG STAY LOWER ARM AND
DRAG STAY LOWER ARM TO MAIN FITTING PIN EXTERNAL
SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS
AND BUSH FLANGES.
322106-02-1
322109-01-1
R
322110-02-2
711 NOSE GEAR
AF
NDT
SDI
SPECIAL DETAILED INSPECTION OF NLG DRAG STAY PINTLE
PIN.
SOURCE
MRB CPCP
REFERENCE
322100-220-815
STRUCTURE : LANDING GEAR
C O N T I N U E D
M/H
APPLICABILITY
1
0.20 ALL
1
1
0.10 ALL
0.10
1
0.20 ALL
1
0.20 ALL
1
1
0.10 ALL
0.10
1
1.70 A330-200
OR
A330-200F
OR
A330-300
OR
MRB REFERENCE:
322103-02-1
MRB CPCP
322100-220-816
MRB REFERENCE:
322104-02-1
MRB CPCP
322100-220-817
MRB REFERENCE:
322105-02-1
MRB CPCP
322100-220-818
MRB REFERENCE:
322106-02-1
MRB CPCP
322100-220-819
MRB REFERENCE:
322109-01-1
MRB CPCP
322100-280-803
MRB REFERENCE:
322110-02-1
NOTE:
* * * * *
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -32
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
322110-02-2
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
PREP.: DISCONNECT DRAG STAY AND REMOVE PINTLE PIN;
322110-02-3
123 NOSE GEAR
NDT
SDI
SPECIAL DETAILED INSPECTION OF NLG DRAG STAY PINTLE
PIN.
*
T:
12 YE
I:
12 YE
MRB CPCP
322100-280-803
1.70 A330-800
POST 208041
OR
A330-900
POST 208041
*
0.17
1
TBD A330-200
OR
A330-200F
OR
A330-300
OR
A330-800
PRE 208041
OR
A330-900
5.00 PRE 208041
MRB REFERENCE:
322110-02-2
PREP.: DISCONNECT DRAG STAY AND REMOVE PINTLE PIN;
322119-01-2
123 NOSE GEAR
AF
DET
DETAILED INSPECTION OF NLG RETRACTION ACTUATOR PIN
(AIRFRAME).
T:
10 YE
I:
10 YE
MRB CPCP
322100-220-827
MRB REFERENCE:
322119-01-1
NOTE:
PLANNING:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF LDG
REMOVAL.
PREP.: RETRACTION ACTUATOR REMOVED;
N
322119-01-3
123 NOSE GEAR
*
AF
DET
DETAILED INSPECTION OF NLG RETRACTION ACTUATOR PIN
(AIRFRAME).
T:
12 YE
I:
12 YE
MRB CPCP
322100-220-827
A330-800
PRE 208041
OR
0.17 A330-900
PRE 208041
1
NOTE:
TASK TO BE PERFORMED AT THE OPPORTUNITY OF LDG
REMOVAL.
R
APPLICABILITY
* * * * *
TASK TO BE PERFORMED AT THE OPPORTUNITY OF LDG
REMOVAL.
N
M/H
1
MRB REFERENCE:
322119-01-2
TBD A330-800
POST 208041
OR
A330-900
POST 208041
NOTE:
PLANNING:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF LDG
REMOVAL.
PREP.: RETRACTION ACTUATOR REMOVED;
* * * * *
STRUCTURE : LANDING GEAR
E N D
*
5.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -32
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
521103-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
831 FWD PASSENGER/CREW DOOR
AF
841
GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD
PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.
GVI
T:
8500 FC
I:
8500 FC
SOURCE
ALI
MRB
REFERENCE
521100-210-801
MEN
M/H
APPLICABILITY
1
1
0.15 A330-200F
0.15
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-900
1
1
0.60 ALL
0.60
PREP.: ESCAPE SLIDE;
INSULATION;
LINING;
*
0.28
ACCESS: 831
841
*
*
0.02
0.02
1
1
0.10 GROUP
0.10 OR
GROUP
OR
GROUP
OR
GROUP
0.28 OR
GROUP
ALI REFERENCE:
521103-01-02
MRB REFERENCE:
521103-01-3
521103-01-2
521104-01-1
831 FWD PASSENGER/CREW DOOR
AF
841
GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD
PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.
831 FWD PASSENGER/CREW DOOR
AF
DET
841
DETAILED INSPECTION OF DOOR 1 (FORWARD PASSENGER/CREW
DOOR), INTERNAL STRUCTURE.
TPS
521105-01-1
STRUCTURE : DOORS
GVI
T: 12800 FC
ALI
I: 12800 FC
T:
6 YE
I:
6 YE
521100-210-801
ALI REFERENCE:
521103-01-02
MRB CPCP
521100-200-801
MRB REFERENCE:
521104-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
831 FWD PASSENGER/CREW DOOR
AF
DET
841
DETAILED INSPECTION OF TOP & BOTTOM CROSSBEAMS T8 &
T1 ENDS AT FRAMES FR 1 AND FR 7 IN THEIR UNION TO
DOOR STOP ASSEMBLIES, ON FORWARD PASSENGER/CREW DOOR,
LH/RH.
T: 33900 FC
ALI
I: 15500 FC
521100-220-803
ALI REFERENCE:
521105-01-01
PREP.: ESCAPE SLIDE;
INSULATION;
LINING;
*
ACCESS: 831
841
*
*
REV. DATE: JUL 01/21
SECTION:
3 -52
32A
33A
33B
33C
33D
0.02
0.02
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
521201-01-2
521202-01-1
ZONE
832 MID PASSENGER/CREW DOOR
842
GENERAL VISUAL INSPECTION OF DOOR 2 (MID
PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE
521301-01-2
521302-01-1
GVI
T: 12800 FC
SOURCE
MRB
I: 12800 FC
T:
6 YE
I:
6 YE
REFERENCE
521200-200-803
MEN
521200-200-801
APPLICABILITY
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
1
1
MRB REFERENCE:
521201-01-3
MRB CPCP
M/H
PREP.: DOOR INSULATION;
DOOR LINING;
ESCAPE SLIDE;
*
0.60 A330-200
0.60 OR
A330-300
OR
A330-800
OR
A330-900
0.40
ACCESS: 832
842
*
*
0.02
0.02
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
1
1
MRB REFERENCE:
521202-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
833 AFT PASSENGER/CREW DOOR
AF
843
GENERAL VISUAL INSPECTION OF DOOR 4 (AFT
PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.
GVI
833 AFT PASSENGER/CREW DOOR
AF
DET
843
DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW
DOOR), INTERNAL STRUCTURE.
T: 12800 FC
MRB
I: 12800 FC
T:
6 YE
I:
6 YE
521300-200-803
MRB REFERENCE:
521301-01-3
PREP.: ESCAPE SLIDE;
INSULATION;
LINING;
*
0.60 A330-200
0.60 OR
A330-300
OR
A330-800
OR
A330-900
0.28
ACCESS: 833
*
0.02
TPS
MRB CPCP
521300-200-801
MRB REFERENCE:
521302-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
* * * * *
STRUCTURE : DOORS
AF
832 MID PASSENGER/CREW DOOR
AF
DET
842
DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW
DOOR), INTERNAL STRUCTURE.
TPS
R
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
521302-01-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
522201-01-2
522202-01-1
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
844
GENERAL VISUAL INSPECTION OF DOOR 3
(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL
SURFACE.
523101-01-2
GVI
*
0.02
MRB
T:
6 YE
I:
6 YE
522200-200-807
1
1
0.15 A330-200
0.15 OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
522201-01-3
MRB CPCP
522200-200-802
1
1
PREP.: ESCAPE SLIDE;
INSULATION;
LINING;
*
ACCESS: 834
844
*
*
0.02
0.02
1
0.40 A330-200
OR
A330-200F
OR
A330-300
OR
A330-800
OR
A330-900
1
1.00 ALL
MRB REFERENCE:
522202-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
800 FORWARD CARGO COMPARTMENT DOOR
AF
821 FORWARD CARGO COMPARTMENT DOOR
AF
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, INTERNAL STRUCTURE.
* * * * *
STRUCTURE : DOORS
APPLICABILITY
0.40 A330-200
0.40 OR
A330-300
OR
A330-800
OR
A330-900
0.28
GVI
GENERAL VISUAL INSPECTION OF THE FORWARD CARGO
COMPARTMENT DOOR SKIN, EXTERNAL SURFACE.
523102-01-1
T: 12800 FC
I: 12800 FC
834 PASSENGER COMPARTMENT EMERGENCY EXIT
AF
DET
844
DETAILED INSPECTION OF DOOR 3
(EMERGENCY/PASSENGER/CREW DOOR), INTERNAL STRUCTURE.
TPS
R
M/H
* * * * *
843
R
MEN
C O N T I N U E D
DET
T:
5200 FC
I:
5200 FC
T:
12 YE
I:
6 YE
MRB
523100-210-801
MRB REFERENCE:
523101-01-2
MRB CPCP
523100-220-801
MRB REFERENCE:
523102-01-1
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -52
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
523102-01-1
* * * * *
TPS
C O N T I N U E
SOURCE
REFERENCE
821AR
821BR
821CR
821DR
821 FORWARD CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF LATCHING HOOKS OF
FORWARD CARGO COMPARTMENT DOOR (10 PLACES).
ACCESS: 821
R
523104-01-1
523104-01-3
T:
I:
132BR
132HR
132CR
132JR
132DR
132KR
132ER
132LR
132FR
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 132AR
132GR
R
523105-01-1
132BR
132HR
132CR
132JR
132DR
132KR
132ER
132LR
4400 FC
523100-210-804
0.50
*
0.85
1
1.20 A330-200
OR
A330-200F
OR
A330-300
0.40 OR
A330-800
OR
A330-900
MRB REFERENCE:
523103-02-1
12 YE
OR
26800 FC
ALI
MRB
MRB CPCP
12 YE
OR
4400 FC
12 YE
OR
26800 FC
523100-220-802
MRB REFERENCE:
523104-01-1
523104-01-2
MRB
MRB CPCP
523100-220-802
0.40 A330-200
0.40 OR
A330-300
OR
A330-200F
*
0.31
1
1
0.40 A330-800
0.40 OR
A330-900
*
0.31
1
1.00 A330-200
OR
A330-200F
MRB REFERENCE:
523104-01-1
523104-01-2
12 YE
OR
4400 FC
SDI
T:
5400 FC
SPECIAL DETAILED INSPECTION (HFEC) OF ACTUATOR ATTACH
I:
5400 FC
MRB REFERENCE:
REV. DATE: JUL 01/21
SECTION:
C O N T I N U E D
NDT
1
1
ALI REFERENCE:
523104-01-02
132FR
821 FORWARD CARGO COMPARTMENT DOOR
* * * * *
STRUCTURE : DOORS
*
*
132 FORWARD CARGO COMPARTMENT DOOR
AF
DET
821
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR
HINGE ASSEMBLIES AT FR 20B TO FR 25 (10 PLACES).
TPS
MRB
821BR
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 132AR
132GR
N
821AR
T: 26800 FC
I:
132 FORWARD CARGO COMPARTMENT DOOR
AF
DET
821
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR
HINGE ASSEMBLIES AT FR 20B TO FR 25 (10 PLACES).
TPS
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 821
523103-02-1
M/H
* * * * *
PREP.: LINING Z821;
R
MEN
MRB
523100-250-801
* * * * *
3-52
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523105-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
523105-01-1
ACCESS: 821
523105-01-2
*
821 FORWARD CARGO COMPARTMENT DOOR
NDT
SDI
T:
5400 FC
SPECIAL DETAILED INSPECTION (HFEC) OF ACTUATOR ATTACH
FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A.
I:
5400 FC
ALI
523100-250-801
523105-02-1
821 FORWARD CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF ACTUATOR ATTACH FITTING OF
FORWARD CARGO COMPARTMENT DOOR AT FR 22A.
T:
6 YE
I:
6 YE
MRB
523100-220-810
AF
DET
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR
FR 20B, BETWEEN BEAM 3 AND BEAM 4.
T: 10600 FC
I:
ALI
2600 FC
523100-220-804
AF
DET
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR
FR 20B, BETWEEN BEAM 3 AND BEAM 4.
STRUCTURE : DOORS
1
TBD A330-200
OR
A330-200F
OR
A330-300
0.10 OR
A330-800
OR
A330-900
1
*
821 FORWARD CARGO COMPARTMENT DOOR
* * * * *
0.10
ALI REFERENCE:
523106-01-01
ACCESS: 821CR
523106-01-2
*
*
821 FORWARD CARGO COMPARTMENT DOOR
C O N T I N U E D
T: 24600 FC
I:
ALI
523100-220-804
9100 FC
ALI REFERENCE:
523106-01-02
REV. DATE: JUL 01/21
SECTION:
OR
A330-300
0.10 OR
A330-800
OR
A330-900
1.00 A330-800
OR
A330-900
MRB REFERENCE:
523105-02-1
ACCESS: 821
523106-01-1
APPLICABILITY
1
ALI REFERENCE:
523105-01-01
ACCESS: 821
N
M/H
* * * * *
FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A.
R
MEN
1
0.20 A330-200
PRE 50528
PRE 51038
(52-3068)
OR
0.30 A330-300
PRE 50528
PRE 51038
(52-3068)
0.20 A330-200
POST 51038
(52-3068)
OR
A330-300
* * * * *
3 -52
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523106-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
821 FORWARD CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR BEAM
3 AREA BETWEEN FRAME FR 20A AND FR 21, INTERNAL.
523110-01-2
523201-01-2
6900 FC
I:
2500 FC
ALI
523100-210-802
1
0.20 A330-200
PRE 50528
PRE 202700
(52-3105)
PRE 203231
0.50 (52-3110)
OR
0.10 A330-300
PRE 50528
PRE 202700
(52-3105)
PRE 203231
(52-3110)
ALI REFERENCE:
523110-01-01
ACCESS: 821
*
821 FORWARD CARGO COMPARTMENT DOOR
AF
GVI
T: 16600 FC
I:
ALI
2500 FC
523100-210-802
1
ALI REFERENCE:
523110-01-02
PREP.: LINING Z821;
*
ACCESS: 821
*
800 AFT CARGO COMPARTMENT DOOR
AF
GENERAL VISUAL INSPECTION OF THE AFT CARGO
COMPARTMENT DOOR SKIN, EXTERNAL SURFACE.
STRUCTURE : DOORS
T:
0.30 POST 51038
(52-3068)
*
* * * * *
APPLICABILITY
*
PREP.: LINING Z821;
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR BEAM
3 AREA BETWEEN FRAME FR 20A AND FR 21, INTERNAL.
R
M/H
* * * * *
ACCESS: 821CR
523110-01-1
MEN
C O N T I N U E D
GVI
T:
5200 FC
MRB
523200-210-801
I:
5200 FC
MRB REFERENCE:
523201-01-2
REV. DATE: JUL 01/21
SECTION:
1
0.20 A330-200
POST 50528
PRE 202701
(52-3111)
PRE 202702
0.50 OR
A330-200F
0.10 PRE 202701
(52-3111)
PRE 202702
OR
A330-300
POST 50528
PRE 202701
(52-3111)
PRE 202702
0.40 A330-200
OR
A330-200F
OR
A330-300
OR
* * * * *
3 -52
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
523201-01-2
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-800
OR
A330-900
523202-01-1
822 AFT CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE.
TPS
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: LINING Z822;
ACCESS: 822
R
523202-01-2
822AR
822BR
822CR
ALI
MRB CPCP
523200-220-801
AF
DET
6 YE
OR
10100 FC
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE.
T:
12 YE
I:
6 YE
MRB REFERENCE:
523202-01-1
MRB CPCP
523200-220-801
822AR
822BR
822CR
822DR
822 AFT CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF LATCHING HOOKS OF AFT
CARGO COMPARTMENT DOOR.
ACCESS: 822
R
523204-01-1
822AR
T: 26800 FC
I:
MRB
4400 FC
523200-210-803
0.50
*
0.85
1
1.00 A330-200F
OR
A330-800
OR
A330-900
*
0.50
*
0.85
1
1.20 A330-200
OR
A330-200F
OR
A330-300
0.40 OR
A330-800
OR
A330-900
MRB REFERENCE:
523203-02-1
822BR
*
152 AFT CARGO COMPARTMENT DOOR
AF
DET
822
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR
* * * * *
STRUCTURE : DOORS
*
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 822
523203-02-1
1.00 A330-200
OR
A330-300
MRB REFERENCE:
523202-01-1
PREP.: LINING Z822;
R
1
ALI REFERENCE:
523202-01-01
822DR
822 AFT CARGO COMPARTMENT DOOR
TPS
12 YE
OR
32200 FC
C O N T I N U E D
T:
12 YE
OR
26800 FC
ALI
MRB
MRB CPCP
523200-220-802
ALI REFERENCE:
1
1
0.40 A330-200
0.40 OR
A330-300
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
523204-01-1
* * * * *
C O N T I N U E
SOURCE
N
523204-01-3
152DR
152KR
152ER
152LR
I:
152BR
152HR
152CR
152JR
152DR
152KR
152ER
152LR
12 YE
OR
4400 FC
MRB REFERENCE:
523204-01-1
523204-01-2
152FR
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 152AR
152GR
523205-01-1
152CR
152JR
152 AFT CARGO COMPARTMENT DOOR
AF
DET
822
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR
HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES).
TPS
R
152BR
152HR
152FR
822 AFT CARGO COMPARTMENT DOOR
NDT
12 YE
OR
26800 FC
MRB
MRB CPCP
523205-01-2
T:
5400 FC
SPECIAL DETAILED INSPECTION (HFEC) OF ACTUATOR ATTACH
FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A.
I:
5400 FC
MRB
523200-250-801
523205-02-1
STRUCTURE : DOORS
0.32
1
1
0.40 A330-800
0.40 OR
A330-900
*
0.32
1
1.00 A330-200
OR
A330-200F
OR
A330-300
0.10 OR
A330-800
OR
A330-900
*
822 AFT CARGO COMPARTMENT DOOR
SDI
T:
5400 FC
SPECIAL DETAILED INSPECTION (HFEC) OF ACTUATOR ATTACH
FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A.
I:
5400 FC
NDT
822 AFT CARGO COMPARTMENT DOOR
DET
T:
6 YE
DETAILED INSPECTION OF ACTUATOR ATTACH FITTING OF AFT
CARGO COMPARTMENT DOOR AT FR 62A.
I:
6 YE
* * * * *
*
MRB REFERENCE:
523205-01-1
ALI
523200-250-801
C O N T I N U E D
AF
1
1.00 A330-800
OR
A330-900
*
0.10
ALI REFERENCE:
523205-01-01
ACCESS: 822
N
APPLICABILITY
OR
A330-200F
MRB REFERENCE:
523204-01-1
523204-01-2
12 YE
OR
4400 FC
SDI
523200-220-802
ACCESS: 822
R
M/H
523204-01-02
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 152AR
152GR
MEN
* * * * *
HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES).
TPS
REFERENCE
MRB
523200-220-811
MRB REFERENCE:
523205-02-1
1
TBD A330-200
OR
A330-200F
OR
A330-300
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523205-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
822 AFT CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR BEAM 3 AREA
BETWEEN FRAME FR 59A AND FR 60A, INTERNAL.
523211-02-2
T: 33000 FC
I:
ALI
6500 FC
523200-220-810
0.40 GROUP 32A
OR
GROUP 33A
POST 44852
(52-3044)
0.50 OR
GROUP 33B
0.10 POST 44852
(52-3044)
OR
GROUP 33B
POST 44854
OR
GROUP 33C
OR
GROUP 33D
ACCESS: 822
*
AF
DET
T: 12000 FC
I:
ALI
4000 FC
523200-220-810
822 AFT CARGO COMPARTMENT DOOR
1
ALI REFERENCE:
523211-02-02
*
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR FRAME FORK LUG C64A.
T: 19900 FC
I:
ALI
3400 FC
523200-210-804
1
ALI REFERENCE:
523212-01-01
ACCESS: 822BR
STRUCTURE : DOORS
1
ALI REFERENCE:
523211-02-01
PREP.: LINING Z822;
523212-01-1
0.10 OR
A330-800
OR
A330-900
*
DETAILED INSPECTION OF AFT CARGO DOOR BEAM 3 AREA
BETWEEN FRAME FR 59A AND FR 60A, INTERNAL.
R
APPLICABILITY
*
PREP.: LINING Z822;
822 AFT CARGO COMPARTMENT DOOR
M/H
* * * * *
ACCESS: 822
523211-02-1
MEN
*
REV. DATE: JUL 01/21
SECTION:
3-52
0.40 GROUP 33A
PRE 44852
(52-3044)
OR
GROUP 33B
0.50 PRE 44852
(52-3044)
PRE 44854
0.08 A330-200
OR
A330-300
OR
A330-200F
0.15
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
523212-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
822 AFT CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR FRAME FORK LUG C64A.
T: 23900 FC
I:
SOURCE
ALI
3400 FC
REFERENCE
523200-210-804
523301-01-3
800 BULK CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF THE BULK CARGO
COMPARTMENT DOOR SKIN, EXTERNAL SURFACE.
523302-01-1
823 BULK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE.
TPS
523303-01-1
T:
8300 FC
I:
8300 FC
T:
12 YE
I:
6 YE
MRB
523300-210-801
523300-220-801
1
0.20 A330-200
OR
A330-200F
OR
A330-300
OR
A330-800
OR
A330-900
1
0.75 ALL
MRB REFERENCE:
523302-01-1
*
TBD
ACCESS: 823
*
0.05
1
0.20 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
0.05 OR
GROUP
823 BULK CARGO COMPARTMENT DOOR
AF
DET
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
12 YE
OR
34500 FC
ALI
MRB CPCP
523300-220-802
ALI REFERENCE:
523303-01-01
12 YE
OR
4400 FC
MRB REFERENCE:
523303-01-1
ACCESS: 823
*
823 BULK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF STOP FITTINGS ON BULK CARGO
* * * * *
STRUCTURE : DOORS
0.15
PREP.: LINING Z823;
TPS
523303-01-2
*
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
DETAILED INSPECTION OF STOP FITTINGS ON BULK CARGO
COMPARTMENT DOOR.
R
APPLICABILITY
0.08 A330-800
OR
A330-900
MRB REFERENCE:
523301-01-3
MRB CPCP
M/H
1
ALI REFERENCE:
523212-01-02
ACCESS: 822BR
R
MEN
C O N T I N U E D
T:
12 YE
I:
12 YE
MRB CPCP
523300-220-802
MRB REFERENCE:
1
32A
33A
33B
33C
33D
0.20 GROUP 32E
OR
GROUP 32F
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
523303-01-2
* * * * *
C O N T I N U E
SOURCE
523303-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 823
523802-01-1
*
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF MAIN DECK CARGO DOOR INTERNAL
STRUCTURE, EXCLUDING SIDE FRAMES AND ACTUATOR FRAME.
TPS
T:
I:
: TYPE 3 TPS IS TO BE APPLIED.
PREP.: LINING Z835;
523803-01-1
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF MAIN DECK CARGO DOOR ACTUATOR
ATTACH FITTINGS INCLUDING RIVETING.
TPS
12 YE
OR
17000 FC
MRB
MRB CPCP
835 MAIN DECK CARGO COMPARTMENT DOOR
ACCESS: 835BL
AF
12 YE
I:
12 YE
MRB CPCP
523811-220-804
OR
GROUP 33E
OR
GROUP 38E
0.05 OR
GROUP 39E
1
0.50 A330-200F
*
0.70
1
0.10 A330-200F
*
0.70
1
0.30 A330-200F
*
0.24
1
0.20 A330-200F
MRB REFERENCE:
523803-01-1
DET
835 MAIN DECK CARGO COMPARTMENT DOOR
* * * * *
T:
12 YE
I:
12 YE
MRB CPCP
523811-220-806
MRB REFERENCE:
523804-01-1
835CL
AF
GENERAL VISUAL INSPECTION OF MAIN DECK CARGO DOOR
LOCKING MECHANISM, ATTACH FITTINGS AND SUPPORT
STRUCTURE AT ALL FRAMES.
STRUCTURE : DOORS
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
DETAILED INSPECTION OF MAIN DECK CARGO DOOR LOCKING
MECHANISM, ATTACH FITTINGS AND SUPPORT STRUCTURE AT
ALL FRAMES.
523804-02-1
M/H
MRB REFERENCE:
523802-01-1
523802-01-2
12 YE
OR
10600 FC
T:
523811-220-801
PREP.: LINING Z835;
523804-01-1
MEN
* * * * *
COMPARTMENT DOOR.
TPS
REFERENCE
C O N T I N U E D
GVI
T: 17000 FC
I:
MRB
523811-200-802
2500 FC
MRB REFERENCE:
523804-02-1
REV. DATE: JUL 01/21
SECTION:
* * * * *
3-52
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
523804-02-1
ZONE
MEN
M/H
*
0.24
1
0.20 A330-200F
*
0.02
1
0.97 A330-200F
*
0.02
1
0.30 A330-200F
*
0.02
1
0.15 A330-200F
PREP.: LINING Z835;
*
0.70
ACCESS: 835
*
0.02
1
0.15 A330-200
OR
A330-200F
OR
A330-300
* * * * *
ACCESS: 835BL
523805-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
REFERENCE
* * * * *
835CL
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF MAIN DECK CARGO DOOR LATCHING
HOOKS AND BOLTS.
T:
12 YE
I:
12 YE
MRB CPCP
523811-220-805
MRB REFERENCE:
523805-01-1
ACCESS: 835
523805-02-1
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF MAIN DECK CARGO DOOR
LATCHING HOOKS AND BOLTS.
T:
8000 FC
I:
8000 FC
MRB
523811-210-802
MRB REFERENCE:
523805-01-2
ACCESS: 835
523806-01-1
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
DET
T:
DETAILED INSPECTION OF MAIN DECK CARGO DOOR PIANO
HINGE FITTING.
I:
ACCESS: 835
523807-01-1
835 MAIN DECK CARGO COMPARTMENT DOOR
AF
DET
DETAILED INSPECTION OF MAIN DECK CARGO DOOR SIDE
FRAMES AND STOP FITTINGS.
R
524101-01-2
811 AVIONICS COMP ACCESS DOOR
AF
DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER
ACCESS DOOR SKIN, EXTERNAL SURFACE.
* * * * *
STRUCTURE : DOORS
APPLICABILITY
C O N T I N U E D
DET
6 YE
OR
8000 FC
MRB
MRB CPCP
MRB REFERENCE:
523806-01-1
523806-01-2
6 YE
OR
8000 FC
T:
12 YE
I:
12 YE
T: 10300 FC
523811-220-807
MRB CPCP
523811-220-803
MRB REFERENCE:
523807-01-1
ALI
I: 10300 FC
524111-200-801
ALI REFERENCE:
524101-01-02
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
524101-01-2
N
524101-01-3
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
811 AVIONICS COMP ACCESS DOOR
AF
DET
121 AVIONICS COMP ACCESS DOOR
AF
DET
122
811 DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER
ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS
AND HINGE FITTINGS ON FUSELAGE.
TPS
524103-01-2
524103-01-3
REFERENCE
T: 10300 FC
MRB
I: 10300 FC
T:
6 YE
I:
6 YE
524111-200-801
M/H
APPLICABILITY
1
0.15 A330-800
OR
A330-900
1
1
1
0.30 ALL
0.30
0.30
MRB REFERENCE:
524101-01-3
MRB CPCP
524111-200-803
MRB REFERENCE:
524102-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: DOOR FLOOR PANEL;
*
TBD
ACCESS: 811
*
0.05
1
1
1
0.25 GROUP 32A
0.25 PRE 49194
0.25 OR
GROUP 33A
OR
TBD GROUP 33B
OR
0.05 GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
121 AVIONICS COMP ACCESS DOOR
AF
DET
122
811 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS.
T: 10000 FC
I:
ALI
6000 FC
524111-200-805
ALI REFERENCE:
524103-01-02
PREP.: DOOR FLOOR PANEL;
*
ACCESS: 811
*
121 AVIONICS COMP ACCESS DOOR
AF
DET
122
811 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS.
T: 24000 FC
I:
ALI
6000 FC
524111-200-805
ALI REFERENCE:
524103-01-03
PREP.: DOOR FLOOR PANEL;
* * * * *
STRUCTURE : DOORS
MEN
* * * * *
DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER
ACCESS DOOR SKIN, EXTERNAL SURFACE.
524102-01-1
SOURCE
C O N T I N U E D
1
1
1
*
0.25 GROUP 32A
0.25 POST 49194
0.25 OR
GROUP 32E
OR
TBD GROUP 33C
POST 49194
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
524103-01-3
* * * * *
C O N T I N U E
SOURCE
REFERENCE
524103-01-4
528103-01-1
121 AVIONICS COMP ACCESS DOOR
AF
DET
122
811 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS.
T: 24000 FC
I:
MRB
6000 FC
524111-200-805
MRB REFERENCE:
524103-01-4
0.05 OR
GROUP 33D
POST 49194
OR
GROUP 33E
OR
A330-200F
1
1
1
0.25 A330-800
0.25 OR
0.25 A330-900
TBD
ACCESS: 811
*
0.05
1
1
0.20 ALL
0.20
*
*
0.15
0.15
1
1
0.20 A330-200
0.20 OR
A330-200F
OR
A330-300
*
*
0.15
0.15
734 MAIN GEAR DOORS
AF
DET
744
DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR,
FORWARD AND AFT FITTINGS, LH/RH.
T:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
12 YE
OR
31100 FC
MRB CPCP
528100-200-803
MRB REFERENCE:
528103-01-1
12 YE
OR
8900 FC
ACCESS: 734
744
734 MAIN GEAR DOORS
AF
DET
744
DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR,
CENTER FITTING AND SURROUNDING AREA (300 MM AROUND),
LH/RH.
NOTE:
TPS APPLICATION REQUIRED ON FITTING ONLY
TPS
T:
I:
6 YE
OR
8300 FC
ALI
MRB CPCP
6 YE
OR
8300 FC
528100-200-804
ALI REFERENCE:
528104-01-02
MRB REFERENCE:
528104-01-2
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
* * * * *
STRUCTURE : DOORS
*
*
I:
528104-01-2
APPLICABILITY
PREP.: DOOR FLOOR PANEL;
TPS
R
M/H
* * * * *
ACCESS: 811
N
MEN
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -52
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
528104-01-2
N
528104-01-4
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
REFERENCE
T:
I:
NOTE:
TPS APPLICATION REQUIRED ON FITTING ONLY
6 YE
OR
8300 FC
MRB
MRB CPCP
528100-200-804
6 YE
OR
8300 FC
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
6 YE
OR
9600 FC
ALI
MRB CPCP
6 YE
OR
9600 FC
528200-200-806
ALI REFERENCE:
528203-01-02
528203-01-3
713 NOSE GEAR DOORS
AF
DET
714
DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD
DOOR, HINGES (1, 2 & 3) INCLUDING FITTINGS ON
FUSELAGE, LH/RH.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
T:
I:
6 YE
OR
9600 FC
MRB
MRB CPCP
6 YE
OR
9600 FC
528200-200-806
*
*
0.15
0.15
1
1
0.30 A330-200
0.30 OR
A330-300
*
*
0.10
0.10
1
1
0.30 A330-800
0.30 OR
A330-900
*
*
0.10
0.10
MRB REFERENCE:
528203-01-1
528203-01-3
ACCESS: 713
714
STRUCTURE : DOORS
0.20 A330-800
0.20 OR
A330-900
MRB REFERENCE:
528203-01-1
ACCESS: 713
714
R
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
713 NOSE GEAR DOORS
AF
DET
714
DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD
DOOR, HINGES (1, 2 & 3) INCLUDING FITTINGS ON
FUSELAGE, LH/RH.
TPS
M/H
1
1
MRB REFERENCE:
528104-01-2
528104-01-3
ACCESS: 734
744
528203-01-1
MEN
* * * * *
734 MAIN GEAR DOORS
AF
DET
744
DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR,
CENTER FITTING AND SURROUNDING AREA (300 MM AROUND),
LH/RH.
TPS
SOURCE
REV. DATE: JUL 01/21
SECTION:
3-52
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
528206-01-1
ZONE
DESCRIPTION
713 NOSE GEAR DOORS
AF
DET
714
DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD
DOOR, HINGES (1, 2 & 3) INCLUDING FITTINGS ON
FUSELAGE, LH/RH.
TPS
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
6 YE
OR
12000 FC
SOURCE
ALI
MRB CPCP
REFERENCE
528200-200-803
715 NOSE GEAR DOORS
AF
DET
716
DETAILED INSPECTION OF NOSE LANDING GEAR AFT DOOR,
HINGES (4 & 5) INCLUDING FITTINGS ON FUSELAGE, LH/RH.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
* * * * *
STRUCTURE : DOORS
E N D
T:
6 YE
OR
12000 FC
I:
6 YE
OR
12000 FC
M/H
APPLICABILITY
1
1
0.30 A330-200F
0.30
*
*
0.10
0.10
1
1
0.20 A330-200F
0.20
ALI REFERENCE:
528206-01-01
MRB REFERENCE:
528206-01-1
ACCESS: 713
714
528207-01-1
MEN
ALI
MRB CPCP
6 YE
OR
12000 FC
528200-200-805
ALI REFERENCE:
528206-01-01
MRB REFERENCE:
528207-01-1
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -52
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531101-01-1
ZONE
110 MAIN STRUCTURE
DET
T:
6 YE
531104-01-1
AF
DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE
BULKHEAD ATTACHED TO FR 1.
I:
6 YE
531106-01-4
M/H
APPLICABILITY
PREP.: INSULATION PANELS;
RADOME OPENED;
*
0.06
ACCESS: 110AL
*
0.05
1
0.30 ALL
1
2.50 ALL
1
0.15 ALL
1
0.20 GROUP 33A
1
0.20 GROUP 32A
OR
GROUP 33B
OR
GROUP 33C
OR
200 MAIN STRUCTURE
DET
T:
6 YE
DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL
VISIBLE PORTIONS OF FRAMEWORK BETWEEN FR 3 AND FR 10,
LH/RH.
I:
6 YE
AF
T:
12 YE
I:
12 YE
T:
6 YE
I:
6 YE
200 MAIN STRUCTURE
AF
200 MAIN STRUCTURE
AF
200 NOSE FORWARD FUSELAGE
DET
DET
DET
T: 21000 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 9 AND
FR 10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA,
EXTERNAL SURFACE, LH/RH.
I: 10100 FC
AF
200 NOSE FORWARD FUSELAGE
DET
T: 32600 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 9 AND
FR 10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA,
EXTERNAL SURFACE, LH/RH.
I: 10000 FC
* * * * *
STRUCTURE : FUSELAGE
531100-200-801
MEN
MRB REFERENCE:
531101-01-1
: TYPE 3 TPS IS TO BE APPLIED.
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
VISIBLE PORTIONS OF RETAINERS.
531106-01-3
MRB CPCP
REFERENCE
0.80 ALL
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
PORTIONS OF FRAMEWORK COVERED BY RETAINERS.
531105-01-1
SOURCE
1
TPS
531102-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E D
AF
MRB CPCP
531100-220-802
MRB REFERENCE:
531102-01-1
MRB CPCP
531100-200-804
MRB REFERENCE:
531104-01-1
MRB CPCP
531100-200-805
MRB REFERENCE:
531105-01-1
ALI
531100-200-836
ALI REFERENCE:
531106-01-03
ALI
531100-200-836
ALI REFERENCE:
531106-01-04
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 1
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531106-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
GROUP 33D
531106-01-5
531106-01-6
200 NOSE FORWARD FUSELAGE
DET
T: 32600 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 9 AND
FR 10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA,
EXTERNAL SURFACE, LH/RH.
I: 10000 FC
200 NOSE FORWARD FUSELAGE
AF
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 9 AND
FR 10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA,
EXTERNAL SURFACE, LH/RH.
531108-01-1
200 NOSE FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CIRCUMFERENTIAL
JOINT AFT OF FR 18 BETWEEN STR 3 AND STR 12, BUTT
JOINT AND REAR PANEL, LH.
T: 24000 FC
I:
531100-200-836
ALI
531100-200-836
200 NOSE FORWARD FUSELAGE
NDT
SDI
ALI
6600 FC
SPECIAL DETAILED INSPECTION (US) OF CIRCUMFERENTIAL
JOINT AT FR 18 BETWEEN STR 11 AND STR 13, BUTT JOINT
AND REAR PANEL, RH.
T: 28700 FC
531100-270-804
STRUCTURE : FUSELAGE
200 FUSELAGE SKIN BTW FR 10 AND FR 13
AF
ALI
I: 19700 FC
DET
T: 10400 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10
AND FR 13 FROM FLOOR LEVEL TO STR 9 FORWARD, EXTERNAL
SURFACE, LH/RH.
I: 10400 FC
1
0.20 A330-200F
1
1.00 A330-200F
*
0.03
1
0.50 A330-200F
*
0.03
1
0.40 A330-200
OR
A330-300
ALI REFERENCE:
531108-01-01
531100-270-805
ALI REFERENCE:
531109-01-01
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531110-02-2
0.20 GROUP 32E
OR
GROUP 33E
ALI REFERENCE:
531106-01-06
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531109-01-1
1
ALI REFERENCE:
531106-01-04
7900 FC
T: 17400 FC
I:
ALI
ALI
REV. DATE: JUL 01/21
531100-220-843
ALI REFERENCE:
531110-02-02
SECTION:
3 -53
PAGE 2
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531110-02-3
N
531110-02-4
531111-01-2
R
R
531111-01-3
531112-02-1
ZONE
200 FUSELAGE SKIN BTW FR 10 AND FR 13
DET
T: 10100 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10
AND FR 13 FROM FLOOR LEVEL TO STR 9 FORWARD, EXTERNAL
SURFACE, LH/RH.
I: 10100 FC
AF
200 FUSELAGE SKIN BTW FR 10 AND FR 13
DET
T: 10400 FC
DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10
AND FR 13 FROM FLOOR LEVEL TO STR 9 FORWARD, EXTERNAL
SURFACE, LH/RH.
I: 10400 FC
AF
200 NOSE FORWARD FUSELAGE
AF
SOURCE
ALI
REFERENCE
531100-220-843
MRB
531100-220-843
7000 FC
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR
10 AND FR 18 FROM STR 9 (FORWARD AND AFT) TO CROWN
CENTERLINE, EXTERNAL SURFACE, LH/RH.
I:
7000 FC
GVI
T:
7500 FC
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR
10 AND FR 18 FROM STR 9 (FORWARD AND AFT) TO CROWN
CENTERLINE, EXTERNAL SURFACE, LH/RH.
I:
7500 FC
100 DOOR 1 CUTOUT
AF
DET
200
DETAILED INSPECTION OF FUSELAGE STRUCTURE AROUND DOOR
1 (FORWARD PASSENGER / CREW DOOR), EXTERNAL SURFACE,
BETWEEN FR 13 AND FR 18 FROM LATERAL LONGITUDINAL LAP
JOINT TO STR 9 AFT, LH/RH.
T:
8900 FC
I:
8900 FC
ALI REFERENCE:
531112-02-01
REV. DATE: JUL 01/21
SECTION:
C O N T I N U E D
AF
M/H
APPLICABILITY
1
0.40 A330-200F
1
0.40 A330-800
OR
A330-900
1
0.30 A330-200F
1
0.30 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
1
1
0.25 A330-200
0.25 OR
GROUP 33A
POST 40347
OR
GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
OR
GROUP 33E
OR
A330-800
OR
MRB REFERENCE:
531110-02-3
T:
200 NOSE FORWARD FUSELAGE
MEN
ALI REFERENCE:
531110-02-03
GVI
* * * * *
STRUCTURE : FUSELAGE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MRB
531100-210-817
MRB REFERENCE:
531111-01-2
MRB
531100-210-817
MRB REFERENCE:
531111-01-3
ALI
531100-220-805
* * * * *
3-53
PAGE 3
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531112-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
A330-900
531112-02-2
531112-02-3
531115-01-1
100 DOOR 1 CUTOUT
AF
DET
200
DETAILED INSPECTION OF FUSELAGE STRUCTURE AROUND DOOR
1 (FORWARD PASSENGER / CREW DOOR), EXTERNAL SURFACE,
BETWEEN FR 13 AND FR 18 FROM LATERAL LONGITUDINAL LAP
JOINT TO STR 9 AFT, LH/RH.
T:
8700 FC
I:
8700 FC
100 DOOR 1 CUTOUT
AF
DET
200
DETAILED INSPECTION OF FUSELAGE STRUCTURE AROUND DOOR
1 (FORWARD PASSENGER / CREW DOOR), EXTERNAL SURFACE,
BETWEEN FR 13 AND FR 18 FROM LATERAL LONGITUDINAL LAP
JOINT TO STR 9 AFT, LH/RH.
T:
4100 FC
I:
4100 FC
100 MAIN STRUCTURE
T:
6 YE
I:
6 YE
AF
DET
DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF
INSTALLED) OF DOOR 1 (FORWARD PASSENGER/CREW DOOR)
CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RH.
ALI
531100-220-805
ALI REFERENCE:
531112-02-02
ALI
531100-220-805
100 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF
INSTALLED) OF DOOR 1 (FORWARD PASSENGER/CREW DOOR)
CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RH.
T:
12 YE
I:
6 YE
MRB CPCP
531100-200-812
531116-01-2
STRUCTURE : FUSELAGE
AF
C O N T I N U E D
0.25 GROUP 33A
0.25 PRE 40347
1
1.00 A330-200
PRE 40347
OR
A330-300
PRE 40347
*
0.30
MRB CPCP
531100-200-812
1
1.00 A330-200
POST 40347
OR
A330-200F
OR
A330-300
0.30 POST 40347
OR
A330-800
OR
A330-900
MRB REFERENCE:
531115-01-2
*
100 MAIN STRUCTURE
* * * * *
1
1
MRB REFERENCE:
531115-01-1
PREP.: SCUFF PLATE;
R
0.25 A330-200F
0.25
ALI REFERENCE:
531112-02-03
PREP.: SCUFF PLATE;
531115-01-2
1
1
GVI
T:
5200 FC
MRB
531100-210-820
1
0.20 A330-200
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 4
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531116-01-2
* * * * *
C O N T I N U E
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND JOINT
SURFACES BETWEEN FR 0 AND FR 18/19 BELOW CABIN FLOOR
LEVEL, EXTERNAL SURFACE.
531117-01-1
SOURCE
121 AVIONICS COMPARTMENT
AF
GVI
122
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BETWEEN FR 1 AND FR 20, FROM CABIN FLOOR
LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL, INCLUDING
CABIN FLOOR SUPPORT STRUCTURE AND NOSE LANDING GEAR
BAY PANELS AND BEAMS.
I:
5200 FC
T:
12 YE
I:
12 YE
MRB REFERENCE:
531116-01-2
MRB CPCP
531100-210-805
MRB REFERENCE:
531117-01-1
A330-300
OR
A330-800
OR
A330-900
1
1
0.50 ALL
0.50
NOTE:
TPS APPLICATION REQUIRED ONLY BETWEEN FR 10 AND FR
20, EXCLUDING NOSE LANDING GEAR BAY PANELS.
TPS
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: AVIONICS COMPARTMENT FLOOR PANELS;
INSULATION TO BE DISPLACED AS REQUIRED;
R
531118-01-1
100 NOSE FORWARD FUSELAGE
GVI
T:
4200 FC
GENERAL VISUAL INSPECTION OF GROUND SERVICES
CONNECTION ACCESS DOORS CUTOUTS AND NOSE LANDING GEAR
CUTOUT, BETWEEN FR 4 AND FR 19 ON LOWER FUSELAGE.
I:
4200 FC
ACCESS: 121AL
531119-01-1
121EL
AF
*
713
AF
GVI
GENERAL VISUAL INSPECTION OF GROUND SERVICES
CONNECTION ACCESS DOORS CUTOUTS, NOSE LANDING GEAR
CUTOUT BETWEEN FR 4 AND FR 19, WASTE, RINSE AND GRU
DOUBLERS ON THE FUSELAGE.
STRUCTURE : FUSELAGE
125AZ
531100-200-863
125EL
126AZ
713
714
T:
3100 FC
I:
3100 FC
1
*
0.30 A330-200
OR
A330-300
OR
A330-800
OR
0.26 A330-900
1
0.30 A330-200F
*
0.91
ALI REFERENCE:
531118-01-01
714
100 NOSE FORWARD FUSELAGE
ACCESS: 121AL
ALI
ALI
531100-210-819
ALI REFERENCE:
531119-01-01
811
REV. DATE: JUL 01/21
TBD
SECTION:
3-53
PAGE 5
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531120-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
123 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY
INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS.
TPS
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
ACCESS: 713
FH OPTIMIZED:
T:
6 YE
OR
1600 FC
OR
11100 FH
I:
714
SOURCE
ALI
MRB CPCP
REFERENCE
531100-210-801
MEN
M/H
APPLICABILITY
1
0.40 A330-200
OR
A330-300
*
0.20
1
0.40 A330-200F
*
0.20
1
0.40 A330-900
*
0.20
ALI REFERENCE:
531120-01-02
MRB REFERENCE:
531120-01-1
6 YE
OR
1600 FC
OR
11100 FH
FC OPTIMIZED:
T:
6 YE
OR
1800 FC
531120-01-2
123 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY
INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS.
TPS
531120-01-3
6 YE
OR
1800 FC
T:
6 YE
OR
1500 FC
I:
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
ACCESS: 713
R
I:
AF
GVI
T:
GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY
INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS.
I:
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
ACCESS: 713
STRUCTURE : FUSELAGE
531100-210-801
MRB REFERENCE:
531120-01-1
531120-01-3
6 YE
OR
1500 FC
714
123 MAIN STRUCTURE
TPS
MRB
MRB CPCP
6 YE
OR
1800 FC
ALI
MRB CPCP
6 YE
OR
1800 FC
531100-210-801
ALI REFERENCE:
531120-01-03
MRB REFERENCE:
531120-01-1
714
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 6
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
531120-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
123 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY
INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS.
TPS
6 YE
OR
1800 FC
ALI
MRB CPCP
REFERENCE
531100-210-801
6 YE
OR
1800 FC
T:
12 YE
I:
12 YE
MRB CPCP
531100-220-803
*
0.20
1
1
0.30 ALL
0.30
GVI
T:
12 YE
I:
12 YE
MRB CPCP
531100-210-802
1
1
TBD
0.20 ALL
0.20
MRB REFERENCE:
531122-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
*
T:
6 YE
I:
6 YE
MRB CPCP
531100-220-804
MRB REFERENCE:
531123-01-1
1
1
TBD
0.50 IF GALLEYS/ TOILETS
0.50 INSTALLED BETWEEN
FR 10 AND FR 13A
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
* * * * *
STRUCTURE : FUSELAGE
0.40 A330-800
*
121 MAIN STRUCTURE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BELOW GALLEYS AND TOILETS FROM CABIN FLOOR LEVEL TO
AVIONICS COMPARTMENT FLOOR LEVEL BETWEEN FR 10 AND FR
13A, LH/RH.
TPS
1
MRB REFERENCE:
531121-01-1
PREP.: AVIONICS COMPARTMENT FLOOR PANELS;
531123-01-1
APPLICABILITY
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
121 MAIN STRUCTURE
AF
122
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BETWEEN FR 1 AND FR 10 BELOW AVIONICS
COMPARTMENT FLOOR LEVEL.
TPS
M/H
MRB REFERENCE:
531120-01-1
PREP.: AVIONICS COMPARTMENT FLOOR PANELS;
531122-01-1
MEN
ALI REFERENCE:
531120-01-03
714
121 MAIN STRUCTURE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BETWEEN FR 10 AND FR 20 BELOW AVIONICS COMPARTMENT
FLOOR LEVEL.
TPS
I:
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
ACCESS: 713
531121-01-1
T:
SOURCE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 7
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531123-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
123 NOSE FORWARD FUSELAGE
AF
*
DET
DETAILED INSPECTION OF NOSE LANDING GEAR BAY SIDE
PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR BAY
FORWARD PANEL TO NOSE LANDING GEAR BAY AFT PANEL,
LH/RH.
ACCESS: 713
FH OPTIMIZED:
T: 38100 FC
ALI WFD
531100-200-835
1
ALI REFERENCE:
531124-01-04
I: 18900 FC
FC OPTIMIZED:
T: 38100 FC
714
*
I: 18900 FC
R
531124-01-6
123 NOSE FORWARD FUSELAGE
AF
DET
DETAILED INSPECTION OF NOSE LANDING GEAR BAY SIDE
PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR BAY
FORWARD PANEL TO NOSE LANDING GEAR BAY AFT PANEL,
LH/RH.
ACCESS: 713
D
531124-01-7
531125-02-1
APPLICABILITY
714
FH OPTIMIZED:
T: 42100 FC
ALI WFD
531100-200-835
1
ALI REFERENCE:
531124-01-06
I: 18900 FC
FC OPTIMIZED:
T: 42100 FC
*
I: 18900 FC
TBD
0.50 GROUP 32A
PRE 49194
OR
GROUP 33A
OR
GROUP 33B
OR
0.20 GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
0.50 GROUP 32A
POST 49194
OR
GROUP 32E
OR
GROUP 33C
POST 49194
0.20 OR
GROUP 33D
POST 49194
OR
GROUP 33E
OR
A330-200F
OR
A330-800
OR
A330-900
************** TASK DELETED **************
121 NOSE FORWARD FUSELAGE
AF
DET
122
DETAILED INSPECTION OF FR 17 ATTACHMENT TO BOTTOM
* * * * *
STRUCTURE : FUSELAGE
M/H
* * * * *
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
531124-01-4
MEN
C O N T I N U E D
T: 18200 FC
ALI
I: 16700 FC
531100-220-868
1
1
0.10 A330-200F
0.10
ALI REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 8
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531125-02-1
* * * * *
C O N T I N U E
SOURCE
MEN
M/H
APPLICABILITY
* * * * *
SKIN FROM STR 48 TO 51, LH/RH.
531125-09-1
REFERENCE
531125-02-01
PREP.: AVIONICS COMPARTMENT PANELS;
*
TBD
ACCESS: 811
821
*
*
0.05
0.10
1
1
0.31 A330-200
0.31 PRE 49194
OR
A330-300
PRE 49194
121 NOSE FORWARD FUSELAGE
NDT
122
SPECIAL DETAILED INSPECTION (HFEC) OF FR 17
ATTACHMENT TO BOTTOM SKIN FROM STR 48 TO STR 51,
LH/RH.
SDI
T:
18 YE
NOTE
I:
6 YE
NOTE
MRB FMP
531100-200-859
MRB REFERENCE:
531125-09-1
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
531126-01-1
PREP.: AVIONICS COMPARTMENT PANELS;
*
TBD
ACCESS: 811
*
0.15
1
0.20 ALL
*
0.20
1
0.15 ALL
123 MAIN STRUCTURE
DET
T:
12 YE
DETAILED INSPECTION OF NOSE LANDING GEAR BAY AFT SIDE
PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, LH/RH.
I:
12 YE
TPS
AF
AF
DET
DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR
FITTING.
MRB REFERENCE:
531126-01-1
T:
12 YE
I:
12 YE
MRB CPCP
531100-200-819
MRB REFERENCE:
531129-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
* * * * *
STRUCTURE : FUSELAGE
531100-200-817
714
123 MAIN STRUCTURE
TPS
MRB CPCP
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 713
531129-01-1
821
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 9
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531129-01-1
531129-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: NOSE LANDING GEAR ACTUATOR DISCONNECTED;
*
1.00
ACCESS: 713
*
0.20
1
0.75 GROUP 32A
PRE 49194
OR
GROUP 33A
OR
1.00 GROUP 33B
OR
0.20 GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
* * * * *
C O N T I N U E
531131-01-2
REFERENCE
714
123 MAIN STRUCTURE
APPLICABILITY
* * * * *
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF NOSE LANDING
GEAR ACTUATOR FITTING.
531130-01-2
SOURCE
T: 32900 FC
I:
ALI
4700 FC
531100-200-861
ALI REFERENCE:
531129-02-02
PREP.: NOSE LANDING GEAR ACTUATOR DISCONNECTED;
*
ACCESS: 713
*
714
121 NOSE FORWARD FUSELAGE
NDT SDI
122
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 16A AT CABIN FLOOR LEVEL, LH/RH.
T: 21900 FC
1
1
0.40 GROUP 33A
0.40 OR
GROUP 33B
PRE 44258
PREP.: INSULATION Z220;
*
4.00
ACCESS: 221GF
222GF
*
*
2.90
2.90
1
1
0.20 GROUP 33A
0.20 OR
GROUP 33B
PRE 44258
*
4.00
I:
ALI
4300 FC
531100-200-845
ALI REFERENCE:
531130-01-02
221HF
222HF
121 NOSE FORWARD FUSELAGE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 16A JOINT AREA BETWEEN STR 28 AND STR 30, LH/RH.
T: 18500 FC
I:
ALI
9800 FC
531100-220-808
ALI REFERENCE:
531131-01-02
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
531131-02-2.
PREP.: INSULATION Z220;
LINING Z220;
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 10
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531131-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
121 NOSE FORWARD FUSELAGE
NDT SDI
122
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, FR 16A JOINT AREA BETWEEN STR 28
AND STR 30, LH/RH.
T: 18500 FC
I:
SOURCE
ALI
9800 FC
REFERENCE
531100-250-803
MEN
M/H
APPLICABILITY
1
1
0.40 GROUP 33A
0.40 OR
GROUP 33B
PRE 44258
*
4.00
1
1
0.20 GROUP 32A
0.20 PRE 49194
OR
GROUP 33A
OR
TBD GROUP 33B
OR
GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
ALI REFERENCE:
531131-02-02
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
531131-01-2
PREP.: INSULATION Z220;
LINING Z220;
531132-01-2
121 NOSE FORWARD FUSELAGE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 14 JOINT BETWEEN STR 28 AND 30 LEVEL, LH/RH.
T: 35100 FC
ALI
I: 12900 FC
531100-220-809
ALI REFERENCE:
531132-01-02
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
531132-01-4
*
121 NOSE FORWARD FUSELAGE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 14 JOINT AREA BETWEEN STR 28 AND STR 30 LEVEL,
LH/RH.
T: 35500 FC
MRB
I: 17400 FC
531100-220-809
MRB REFERENCE:
531132-01-4
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
R
531135-01-2
200 COCKPIT WINDOW FRAME
NDT
*
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF REAR LOWER
CORNER OF THE COCKPIT LATERAL WINDOW FRAME, FORWARD
OF FR 10, EXTERNAL SURFACE, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
1
1
T:
4500 FC
ALI
531100-220-806
I:
4500 FC
ALI REFERENCE:
531135-01-02
REV. DATE: JUL 01/21
SECTION:
1
0.20 GROUP 32A
0.20 POST 49194
OR
GROUP 33C
POST 49194
OR
TBD GROUP 33D
POST 49194
0.80 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
* * * * *
3-53
PAGE 11
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
531135-01-2
531135-01-3
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
200 COCKPIT WINDOW FRAME
REFERENCE
NDT
SDI
221 NOSE FORWARD FUSELAGE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 12 AND 13 DOUBLER AREA AT CROWN CENTERLINE.
T:
4800 FC
I:
4800 FC
T: 17500 FC
ALI
531100-220-806
ALI
I: 10100 FC
531100-220-811
221 NOSE FORWARD FUSELAGE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 12 AND 13 DOUBLER AREA AT CROWN CENTERLINE.
123 NOSE FORWARD FUSELAGE
T: 40000 FC
0.80 A330-200F
1
1
0.10 GROUP 33A
0.10 PRE 42481
*
4.70
ALI
I: 10100 FC
531100-220-811
1
1
0.10 A330-200
0.10 OR
GROUP 33A
POST 42481
OR
4.70 GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
OR
GROUP 33E
ALI REFERENCE:
531136-01-03
AF
DET
T:
12 YE
I:
12 YE
MRB CPCP
531100-220-836
1
0.20 ALL
*
0.20
MRB REFERENCE:
531137-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 713
STRUCTURE : FUSELAGE
1
*
DETAILED INSPECTION OF NOSE LANDING GEAR DRAG STRUT
FITTING ATTACHMENTS TO UPPER AND FORWARD CANTED
PANEL.
TPS
APPLICABILITY
ALI REFERENCE:
531136-01-02
PREP.: CEILING PANELS Z220;
INSULATION Z220;
531137-01-1
M/H
ALI REFERENCE:
531135-01-03
PREP.: CEILING PANELS Z220;
INSULATION Z220;
531136-01-3
MEN
* * * * *
SPECIAL DETAILED INSPECTION (HFEC) OF REAR LOWER
CORNER OF THE COCKPIT LATERAL WINDOW FRAME, FORWARD
OF FR 10, EXTERNAL SURFACE, LH/RH.
531136-01-2
SOURCE
714
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 12
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531138-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
110 NOSE FORWARD FUSELAGE
AF
DET
DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD
FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50
ABOVE COCKPIT FLOOR LEVEL.
T: 34700 FC
I:
SOURCE
ALI
9100 FC
REFERENCE
531100-220-812
531140-01-1
*
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FORWARD PRESSURE BULKHEAD AFT FACE, VERTICAL BEAMS
AND UPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE
COCKPIT FLOOR LEVEL.
T: 34700 FC
I:
ALI
9100 FC
531100-220-813
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
*
ACCESS: 811
*
121 NOSE FORWARD FUSELAGE
NDT SDI
122
211 SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL FR 10
212 AT FLOOR LEVEL ATTACHMENT, ABOVE COCKPIT FLOOR,
INTERNAL STRUCTURE, LH/RH.
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF LATERAL FR 11 SPLICE ABOVE
COCKPIT FLOOR LEVEL ATTACHMENT, INTERNAL STRUCTURE,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
1
1
ALI REFERENCE:
531139-01-02
T: 15700 FC
I:
ALI
8400 FC
531100-200-847
ALI REFERENCE:
531140-01-01
PREP.: GALLEYS AND TOILETS IF INSTALLED;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531141-01-2
1
ALI REFERENCE:
531138-01-02
PREP.: PROTECTIVE SHIELDS Z110;
RADOME OPENED;
531139-01-2
MEN
C O N T I N U E D
T: 17500 FC
I:
ALI
531100-200-837
8500 FC
ALI REFERENCE:
531141-01-02
REV. DATE: JUL 01/21
SECTION:
M/H
APPLICABILITY
0.20 GROUP 32A
PRE 49194
OR
GROUP 33A
OR
GROUP 33B
1.56 OR
GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
0.50 GROUP 32A
0.50 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
OR
TBD GROUP 33C
PRE 49194
0.05 OR
GROUP 33D
PRE 49194
1
1
1
1
0.20
0.20
0.20
0.20
GROUP 33A
OR
GROUP 33B
PRE 42829
*
0.03
1
1
0.20 GROUP 33A
0.20
* * * * *
3-53
PAGE 13
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531141-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
M/H
*
16.03
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF FR 10 UPPER CURVED MEMBER
BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING,
SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.
T: 34900 FC
I:
ALI
4800 FC
531100-200-838
1
1
ALI REFERENCE:
531142-01-02
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531142-02-2
PREP.: CEILING PANELS;
INSULATION TO BE DISPLACED AS REQUIRED;
531142-02-2
211 NOSE FORWARD FUSELAGE
NDT SDI
212
SPECIAL DETAILED INSPECTION (HFEC) OF FR 10 UPPER
CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER
LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL
STRUCTURE, LH/RH.
*
T: 34900 FC
I:
ALI
7800 FC
531100-200-848
ALI REFERENCE:
531142-02-02
1
1
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531142-01-2
PREP.: CEILING PANELS;
INSULATION TO BE DISPLACED AS REQUIRED;
531143-01-2
121 NOSE FORWARD FUSELAGE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FLOOR BEAM AND CRUCIFORM FITTING AT FR 14, LH/RH.
*
T: 16600 FC
I:
ALI
5300 FC
531100-220-837
REV. DATE: JUL 01/21
0.50 GROUP 32A
0.50 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
OR
GROUP 33C
PRE 49194
TBD OR
GROUP 33D
PRE 49194
0.50 GROUP 32A
0.50 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
OR
GROUP 33C
PRE 49194
OR
TBD GROUP 33D
PRE 49194
1
1
0.30 GROUP 33A
0.30 PRE 40347
*
0.38
ALI REFERENCE:
531143-01-02
PREP.: AIR DUCTS;
INSULATION TO BE DISPLACED AS REQUIRED;
VACUUM PIPES;
STRUCTURE : FUSELAGE
APPLICABILITY
* * * * *
PREP.: CREW REST ROOM IF INSTALLED;
GALLEYS AND TOILETS IF INSTALLED;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531142-01-2
MEN
SECTION:
3 -53
PAGE 14
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531144-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
121 NOSE FORWARD FUSELAGE
NDT SDI
122
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, JUNCTION AREA BETWEEN FR 14 AND CRUCIFORM
FITTING, LH/RH.
T: 16600 FC
I:
SOURCE
ALI
7000 FC
REFERENCE
531100-200-849
531145-01-1
221DW
222DW
221GF
222GF
811
122 NOSE FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF
CIRCUMFERENTIAL JOINT AT FR19 BETWEEN STR 45 AND STR
47, BUTT JOINT AND REAR PANEL, RH.
531146-01-1
531147-01-1
APPLICABILITY
0.30 GROUP 33A
0.30 PRE 40347
ALI
I: 23700 FC
531100-250-827
*
TBD
*
*
1.70
1.66
1
0.50 A330-200F
ALI REFERENCE:
531145-01-01
PREP.: AVIONICS COMPARTMENT PANELS;
BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z120;
*
TBD
ACCESS: 122NF
*
0.05
1
1
0.15 GROUP 32A
0.15 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
0.03 OR
GROUP 33C
PRE 49194
0.04 OR
0.04 GROUP 33D
PRE 49194
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FR 7
UPPER MEMBER, LH/RH.
T: 39400 FC
I:
ALI
8600 FC
531100-220-839
ALI REFERENCE:
531146-01-01
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
*
ACCESS: 211JC
212JC
*
*
121 NOSE FORWARD FUSELAGE
NDT SDI
122
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
INTERNAL STRUCTURE, JUNCTION AREA AT FR 14 BETWEEN
FLOOR BEAM AND CRUCIFORM FITTING, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
T: 24400 FC
1
1
M/H
ALI REFERENCE:
531144-01-02
PREP.: INSULATION Z120;
ACCESS: 221AW
222AW
MEN
C O N T I N U E D
T: 35100 FC
ALI
I: 20100 FC
531100-250-828
1
1
0.25 GROUP 33A
0.25 PRE 40347
ALI REFERENCE:
531147-01-01
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 15
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531147-01-1
531148-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
*
TBD
ACCESS: 811
*
0.05
1
0.50 A330-200F
121 NOSE FORWARD FUSELAGE
NDT
SDI
T: 27700 FC
ALI
I: 11400 FC
531100-250-824
ALI REFERENCE:
531148-01-01
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS INCLUDING
TOP 3 NUTS ON CENTRE POST.
*
T: 39300 FC
I:
ALI
8500 FC
531100-220-838
1
1
ALI REFERENCE:
531149-01-01
PREP.: INSULATION Z210;
*
ACCESS: 211AC
*
211AW
211BW
211 NOSE FORWARD FUSELAGE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS INCLUDING
TOP 3 NUTS ON CENTER POST.
T:
18 YE
NOTE
I:
NOTE
MRB FMP
531100-220-838
* * * * *
C O N T I N U E D
0.10 GROUP
0.10 OR
GROUP
OR
GROUP
OR
4.00 GROUP
OR
0.19 GROUP
32A
33A
33B
33C
33D
0.03 GROUP 32A
0.03 POST 49194
OR
GROUP 33C
POST 49194
OR
GROUP 33D
POST 49194
*
4.00
MRB REFERENCE:
531149-09-1
PREP.: INSULATION Z210;
TBD
1
1
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
STRUCTURE : FUSELAGE
APPLICABILITY
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z120;
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z120;
531149-09-1
M/H
* * * * *
SPECIAL DETAILED INSPECTION (US) OF CIRCUMFERENTIAL
JOINT AT FR 18 BETWEEN STR 30 AND STR 33, BUTT JOINT
AND LATERAL PANELS, LH.
531149-01-1
MEN
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 16
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
MEN
M/H
*
0.19
1
1
0.50 ALL
0.50
PREP.: ACCESS BETWEEN FR 1 AND FR 2 FROM AVIONIC
COMPARTMENT;
INSULATION TO BE DISPLACED AS REQUIRED;
*
0.02
ACCESS: 311VU
*
1.25
1
1
0.50 ALL
0.50
*
0.20
531149-09-1
* * * * *
ACCESS: 211AC
531150-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
211AW
SOURCE
REFERENCE
APPLICABILITY
* * * * *
211BW
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD ABOVE FLOOR LEVEL, INCLUDING FR 1, AS FAR AS
VISIBLE.
T:
12 YE
I:
12 YE
MRB CPCP
531100-200-820
MRB REFERENCE:
531150-01-1
NOTE:
IF CORROSION IS FOUND ON THE LOWER PART OF THE
PRESSURE BULKHEAD (SEE 531151-01-1), THE COMPLETE AFT
FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED AND
ELECTRONIC DEVICE REMOVED.
TPS
531151-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
312VU
313VU
314VU
811
121 MAIN STRUCTURE
AF
DET
122
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR PANELS,
INCLUDING FR 1 AND STRINGER CONNECTIONS.
T:
12 YE
I:
6 YE
MRB CPCP
531100-200-829
MRB REFERENCE:
531151-01-1
NOTE:
IF CORROSION IS FOUND ON THE LOWER PART OF THE
PRESSURE BULKHEAD (SEE 531150-01-1), THE COMPLETE AFT
FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED AND
ELECTRONIC DEVICE REMOVED.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: AVIONICS COMPARTMENT FORWARD FLOOR PANELS;
INSULATION TO BE DISPLACED AS REQUIRED;
WIRING BUNDLES DISPLACED;
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 17
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531152-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
211 MAIN STRUCTURE
AF
212
DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND
CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND
FORWARD).
DET
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531154-01-2
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING
PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST,
INTERNAL STRUCTURE, LH/RH.
ST:
12 YE
T:
24 YE
SI:
12 YE
I:
12 YE
T: 15800 FC
I:
SOURCE
MRB CPCP
REFERENCE
531100-200-821
531154-01-3
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING
PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST,
INTERNAL STRUCTURE, LH/RH.
ALI
7700 FC
I:
531100-200-857
0.50 ALL
0.50
*
0.03
1
1
0.50 GROUP 32A
0.50 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
0.05 OR
GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
ALI REFERENCE:
531154-01-02
ALI
7700 FC
531100-200-857
1
1
ALI REFERENCE:
531154-01-03
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
SLIDING WINDOWS OPENED;
STRUCTURE : FUSELAGE
APPLICABILITY
1
1
*
T: 27100 FC
M/H
MRB REFERENCE:
531152-01-1
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
SLIDING WINDOWS OPENED;
R
MEN
*
REV. DATE: JUL 01/21
SECTION:
3 -53
0.50 GROUP 32A
0.50 POST 49194
OR
GROUP 32E
OR
GROUP 33C
0.05 POST 49194
OR
GROUP 33D
POST 49194
OR
GROUP 33E
OR
A330-200F
OR
A330-800
OR
A330-900
PAGE 18
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531154-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING
PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST,
INTERNAL STRUCTURE, LH/RH.
T:
18 YE
NOTE
I:
NOTE
SOURCE
MRB FMP
REFERENCE
531100-200-857
MEN
0.05 GROUP 32A
0.05 POST 49194
OR
GROUP 33C
POST 49194
OR
GROUP 33D
POST 49194
*
0.05
1
2.20 A330-200
OR
A330-300
*
0.03
1
1
0.10 GROUP 33A
0.10
*
0.03
1
1
0.30 GROUP 32A
0.30 OR
GROUP 33A
OR
GROUP 33B
OR
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
531155-01-5
200 MAIN STRUCTURE
NDT
SDI
T: 35200 FC
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE JOINT AT
FR 14C, FROM STR 9 TO STR 12, LH/RH.
I: 13500 FC
ALI WFD
531100-270-806
APPLICABILITY
1
1
MRB REFERENCE:
531154-09-1
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
SLIDING WINDOWS OPENED;
M/H
ALI REFERENCE:
531155-01-02
NOTE:
INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE
THE INSPECTION
PREP.: LINING;
531157-01-2
233 MAIN STRUCTURE
AF
DET
234
DETAILED INSPECTION OF PASSENGER/CREW DOOR UPPER KEEL
FITTINGS AT FR 17 AND AT STR 12 LEVEL, INTERNAL
STRUCTURE, LH/RH.
T: 31300 FC
I:
ALI
6700 FC
531100-200-858
ALI REFERENCE:
531157-01-02
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531158-01-1
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FR 8 AND
FR 9 UPPER MEMBERS, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
T: 35300 FC
ALI
I: 15500 FC
531100-220-842
ALI REFERENCE:
531158-01-01
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 19
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531158-01-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
0.03 GROUP 33C
OR
GROUP 33D
1
1
0.30 GROUP 32E
0.30 OR
GROUP 33E
*
0.03
1
1
0.75 ALL
0.75
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LAVATORY IF INSTALLED;
LINING;
*
0.03
ACCESS: 831
841
*
*
0.02
0.02
1
1
0.10 A330-200F
0.10 PRE 200582
1
0.40 A330-200F
211 MAIN STRUCTURE
AF
DET
212
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FR 8 AND
FR 9 UPPER MEMBERS, LH/RH.
221 MAIN STRUCTURE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND DOOR 1 (FORWARD PASSENGER / CREW DOOR),
BETWEEN FR 13A AND FR 17 AND BETWEEN FLOOR LEVEL AND
STR 9 (AFT), LH/RH.
TPS
531160-01-1
531163-01-1
T: 35300 FC
ALI
I: 15500 FC
531100-220-842
ALI REFERENCE:
531158-01-01
T:
12 YE
I:
6 YE
MRB CPCP
531100-200-823
MRB REFERENCE:
531159-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
121 MAIN STRUCTURE
NDT SDI
122
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, RADIUS OF LUGS ON UPPER CORNER OF
PORTAL FR 15A, LH/RH.
T:
9900 FC
I:
6300 FC
123 MAIN STRUCTURE
T: 13800 FC
NDT
SPECIAL DETAILED INSPECTION (US & HFEC) OF NOSE
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
*
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531159-01-1
M/H
* * * * *
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
531158-01-2
MEN
C O N T I N U E D
SDI
ALI
531100-250-825
ALI REFERENCE:
531160-01-01
ALI
I: 13800 FC
531100-200-871
ALI REFERENCE:
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 20
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531163-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
123 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF NOSE LANDING
GEAR BAY LATERAL PANELS, JUNCTION TO LOWER FR 17
FITTING, LH/RH.
531164-01-2
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF NOSE LANDING
GEAR BAY LATERAL PANELS, JUNCTION TO LOWER FR 17
FITTING, LH/RH.
531165-01-2
T:
7000 FC
I:
7000 FC
ALI
531100-250-826
15.00
T: 17800 FC
ALI
I: 15900 FC
531100-250-826
PREP.: FORWARD AVIONICS COMPARTMENT DOOR OPENED;
INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 811
FH OPTIMIZED:
T: 28200 FC
OR
191400 FH
0.40 A330-200F
PRE 200582
*
0.20
1
0.40 A330-200F
POST 200582
*
0.20
1
1
*
0.15 GROUP
0.15 OR
GROUP
OR
GROUP
OR
TBD GROUP
OR
GROUP
0.05
1
0.40 A330-200F
ALI REFERENCE:
531164-01-02
714
125 NOSE FORWARD FUSELAGE
NDT SDI
126
SPECIAL DETAILED INSPECTION (US) OF FR 17 INNER
FLANGE FASTENER HOLE AT Y +/-750MM, JUNCTION WITH THE
FITTING, LH/RH.
1
ALI REFERENCE:
531164-01-01
714
123 MAIN STRUCTURE
ACCESS: 713
*
APPLICABILITY
531163-01-01
PREP.: NOSE LANDING GEAR;
ACCESS: 713
M/H
* * * * *
LANDING GEAR MAIN ATTACHMENT BEARING BORE, LH/RH.
531164-01-1
MEN
MRB
531100-270-809
MRB REFERENCE:
531165-01-2
I: 18000 FC
OR
122300 FH
*
FC OPTIMIZED:
T: 36000 FC
32A
33A
33B
33C
33D
I: 26900 FC
OR
83500 FH
531167-01-2
100 NOSE FORWARD FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND JOINT
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
T:
5900 FC
MRB
531100-210-818
I:
5900 FC
MRB REFERENCE:
REV. DATE: JUL 01/21
SECTION:
* * * * *
3 -53
PAGE 21
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531167-01-2
* * * * *
C O N T I N U E
SOURCE
125 NOSE FORWARD FUSELAGE
AF
GVI
126
GENERAL VISUAL INSPECTION OF NOSE FORWARD FUSELAGE
LOWER SKIN AND FAIRING SUBSTRUCTURE, AREA COVERED BY
NOSE FAIRING BETWEEN FR 17 AND FR 22 INCLUDING AFT
FACE OF LOWER FR 17 FITTING, AND AFT FITTINGS, LH/RH.
TPS
125GL
531167-01-2
T:
6 YE
I:
6 YE
MRB CPCP
531100-210-815
1
1
0.10 A330-200F
0.10
*
*
2.57
0.75
1
1
0.15 A330-200F
0.15
*
*
4.70
2.50
1
1
0.30 A330-200F
0.30
*
3.40
MRB REFERENCE:
531168-01-1
125HL
125BL
126CR
125CL
714
125DL
T:
6 YE
I:
6 YE
MRB CPCP
531100-210-814
MRB REFERENCE:
531169-01-1
713
125 NOSE FORWARD FUSELAGE
AF
DET
126
DETAILED INSPECTION OF NOSE FORWARD FUSELAGE LOWER
SKIN AND FAIRING SUBSTRUCTURE, AREA COVERED BY NOSE
FAIRING BETWEEN FR 10 AND FR 17, INCLUDING NOSE
LANDING GEAR BAY LATERAL PANEL EXTERNAL SURFACE, FLAT
PANEL, FR 16A AND FORWARD FACE OF LOWER FR 17
FITTING, LH/RH.
ACCESS: 125AL
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 125AL
126BR
531169-02-1
125FL
125 NOSE FORWARD FUSELAGE
AF
GVI
126
GENERAL VISUAL INSPECTION OF NOSE FORWARD FUSELAGE
LOWER SKIN AND FAIRING SUBSTRUCTURE, AREA COVERED BY
NOSE FAIRING BETWEEN FR 10 AND FR 17, INCLUDING NOSE
LANDING GEAR BAY LATERAL PANEL EXTERNAL SURFACE, FLAT
PANEL, FR 16A AND FORWARD FACE OF LOWER FR 17
FITTING, LH/RH.
TPS
M/H
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 125DL
126FR
531169-01-1
MEN
* * * * *
SURFACE BETWEEN FR 0 AND FR 18/19 BELOW CABIN FLOOR
LEVEL, EXTERNAL SURFACE, EXCLUDING AREA COVERED BY
NOSE FAIRING.
531168-01-1
REFERENCE
125BL
125CL
T: 15600 FC
ALI
I: 15600 FC
531100-220-870
ALI REFERENCE:
531169-02-01
713
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 22
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
531169-02-1
* * * * *
126BR
531171-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
126CR
REFERENCE
714
T:
12 YE
I:
12 YE
MRB CPCP
531100-210-803
MRB REFERENCE:
531171-01-1
M/H
*
2.50
1
1
0.20 ALL
0.20
APPLICABILITY
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FLOOR PANELS Z220;
531172-01-1
MEN
* * * * *
210 MAIN STRUCTURE
AF
GVI
220
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE
EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND
TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 17.
TPS
SOURCE
*
210 MAIN STRUCTURE
AF
DET
220
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW
AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING
DOORS ENTRANCE AREA, FROM FR 10 TO FR 17.
T:
5 YE
I:
5 YE
MRB CPCP
531100-200-865
1
1
MRB REFERENCE:
531172-01-1
17.00
2.00 IF GALLEYS/TOILETS
2.00 INSTALLED FROM FR
10 TO FR 17 AND
NOTE 7 STRUCTURE
SECTION NOT
INCORPORATED
NOTE:
- TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7
OF MPD STRUCTURE SECTION ARE NOT INCORPORATED
TPS
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FCRC (IF INSTALLED);
FLOOR PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
R
531172-02-1
*
210 MAIN STRUCTURE
AF
DET
220
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW
AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING
DOORS ENTRANCE AREA, FROM FR 10 TO FR 17.
T:
6 YE
I:
6 YE
MRB CPCP
531100-220-873
ISI 53.00.00106
MRB REFERENCE:
531172-01-2
NOTE:
- TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
1
1
50.00
2.00 IF GALLEYS/TOILETS
2.00 INSTALLED FROM FR
10 TO FR 17 AND
NOTE 7 STRUCTURE
SECTION
INCORPORATED
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 23
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531172-02-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
50.00
APPLICABILITY
* * * * *
OF MPD STRUCTURE SECTION ARE INCORPORATED
TPS
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FCRC (IF INSTALLED);
FLOOR PANELS Z220;
GALLEYS Z220;
LAVATORIES Z220;
531173-01-1
121 MAIN STRUCTURE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BELOW DOOR 1 (FORWARD PASSENGER / CREW DOOR) FROM
CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR
LEVEL, BETWEEN FR 13A AND FR 17, LH/RH.
TPS
T:
6 YE
I:
6 YE
MRB CPCP
531100-200-826
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
231 MAIN STRUCTURE
AF
DET
232
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT
STGR.14/18/22/24, LH/RH.
*
T: 22700 FC
I:
ALI
7700 FC
531100-200-840
531175-01-4
231 MAIN STRUCTURE
AF
DET
232
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT
STGR.14/18/22/24, LH/RH.
*
T: 27100 FC
I:
ALI
7700 FC
531100-200-840
ALI REFERENCE:
531175-01-04
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
1
1
ALI REFERENCE:
531175-01-03
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING;
R
0.80 ALL
0.80
MRB REFERENCE:
531173-01-1
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
531175-01-3
1
1
1
1
*
TBD
0.50 GROUP
0.50 OR
GROUP
OR
GROUP
OR
0.03 GROUP
OR
GROUP
32A
33A
33B
33C
33D
0.50 A330-200F
0.50 OR
GROUP 32E
OR
GROUP 33E
OR
0.03 A330-800
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 24
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
531175-01-4
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
* * * * *
LINING;
531176-01-1
OR
A330-900
121 MAIN STRUCTURE
GVI
T:
6 YE
GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE BELOW
BATTERIES BETWEEN FR 10A AND FR 11A AND BETWEEN STR
41 AND STR 43, LH.
I:
6 YE
TPS
AF
MRB CPCP
531100-210-804
125 MAIN STRUCTURE
NDT
126
SPECIAL DETAILED INSPECTION (US) OF LONGITUDINAL
JUNCTION CENTRAL AND LATERAL PANELS AT STR 46,
EXTERNAL SURFACE BETWEEN FR 11 TO FR 12A, LH/RH.
125BL
126CR
SDI
T: 17400 FC
ALI
I: 17400 FC
531100-270-807
ALI REFERENCE:
531177-01-01
125CL
125 MAIN STRUCTURE
AF
DET
126
DETAILED INSPECTION OF Y750 AFT FITTING, TOP RADIUS,
LH/RH.
T: 23100 FC
ALI
I: 13000 FC
531100-220-871
125 MAIN STRUCTURE
NDT
126
SPECIAL DETAILED INSPECTION (US) OF LOWER FR 17
FITTING AT Y750 FITTING JUNCTION, LH/RH.
SDI
T: 11900 FC
I:
ALI
6700 FC
531100-270-808
ALI REFERENCE:
531179-01-01
ACCESS: 125CL
126CR
STRUCTURE : FUSELAGE
*
0.03
1
1
0.20 A330-200F
0.20
*
*
3.30
2.40
1
1
0.10 A330-200F
0.10
*
*
1.20
1.20
1
1
0.25 A330-200F
0.25
*
*
1.20
1.20
ALI REFERENCE:
531178-01-01
ACCESS: 125CL
126CR
531179-01-1
0.30 ALL
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
ACCESS: 125AL
126BR
531178-01-1
1
MRB REFERENCE:
531176-01-1
PREP.: FWD AVIONICS COMPARTMENT DOOR OPENED;
INSULATION TO BE DISPLACED AS REQUIRED;
531177-01-1
APPLICABILITY
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 25
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531182-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
100 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF INTER-STRINGER
AREA AT CIRCUMFERENTIAL JUNCTION AT FR 18/FR 19 FROM
STR 43 TO STR 47 RH/LH.
531183-01-1
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD
OF FR 13, BELOW STR 9 FORWARD, LH/RH.
T: 40000 FC
SOURCE
ALI
I: 14800 FC
T: 31500 FC
REFERENCE
531100-250-829
ALI
I: 10400 FC
531100-250-821
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD
OF FR 13, BELOW STR 9 FORWARD, LH/RH.
T: 28700 FC
I:
9600 FC
531100-250-821
ALI REFERENCE:
531183-01-02
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z220;
TOILETS;
531183-01-5
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
1
1
0.40 GROUP 33A
0.40 PRE 40347
PRE 55534
(53-3164)
*
10.00
1
1
0.40 GROUP 32A
0.40 PRE 55534
(53-3164)
OR
GROUP 33A
POST 40347
10.00 PRE 55534
(53-3164)
OR
GROUP 33B
PRE 55534
(53-3164)
OR
GROUP 33C
PRE 55534
(53-3164)
OR
GROUP 33D
PRE 55534
(53-3164)
*
T: 28700 FC
I:
ALI
531100-250-821
9600 FC
ALI REFERENCE:
531183-01-02
REV. DATE: JUL 01/21
SECTION:
APPLICABILITY
8.50 A330-200
OR
A330-300
ALI REFERENCE:
531183-01-01
ALI
M/H
1
ALI REFERENCE:
531182-01-01
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z220;
TOILETS;
531183-01-2
MEN
1
1
0.40 GROUP 32E
0.40 PRE 55534
(53-3164)
OR
* * * * *
3 -53
PAGE 26
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531183-01-5
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z220;
TOILETS;
*
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD
OF FR 13, BELOW STR 9 FORWARD, LH/RH.
T: 28800 FC
I:
ALI
8600 FC
531100-250-821
531184-09-1
200 MAIN STRUCTURE
*
SDI
T: 21100 FC
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
EXTERNAL STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL
LAP JOINT (STR 9 AFT LEVEL) FROM FR 13 TO FR 13A AND
FROM FR 14 TO FR 16A, LH/RH.
I: 16900 FC
200 MAIN STRUCTURE
NDT
NDT
1
1
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
EXTERNAL STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL
LAP JOINT (STR 9 AFT LEVEL) FROM FR 13 TO FR 13A AND
FROM FR 14 TO FR 16A, LH/RH.
T:
18 YE
NOTE
I:
6 YE
NOTE
GROUP 32E
PRE 53102
10.00 OR
GROUP 33E
PRE 55534
(53-3164)
OR
GROUP 33E
PRE 53102
0.70 A330-200F
0.70 PRE 201656
ALI REFERENCE:
531183-01-06
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z220;
TOILETS;
531184-01-3
APPLICABILITY
* * * * *
OF FR 13, BELOW STR 9 FORWARD, LH/RH.
531183-01-6
M/H
ALI
531100-250-806
10.00
1
0.40 A330-200F
1
2.80 A330-200
PRE 49194
OR
A330-300
PRE 49194
ALI REFERENCE:
531184-01-03
MRB FMP
531100-250-806
MRB REFERENCE:
531184-09-1
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 27
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531186-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 13, 8 FASTENERS OF
FORWARD UPPER PANEL ABOVE STR 9 FORWARD, LH/RH.
T: 31500 FC
SOURCE
ALI WFD
I: 10400 FC
REFERENCE
531100-200-851
223 MAIN STRUCTURE
NDT SDI
224
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 13, 8 FASTENERS OF
FORWARD UPPER PANEL ABOVE STR 9 FORWARD, LH/RH.
T: 28700 FC
I:
ALI WFD
9600 FC
531100-200-851
ALI REFERENCE:
531186-01-03
PREP.: BOLTS;
DOOR FRAME LININGS Z220;
INSULATION Z220;
LAVATORIES Z220;
531188-01-2
531188-01-3
T: 37000 FC
100 MAIN STRUCTURE
NDT
200
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
T: 33300 FC
STRUCTURE : FUSELAGE
C O N T I N U E D
SDI
I:
I:
ALI WFD
4700 FC
531100-200-868
M/H
APPLICABILITY
0.90 GROUP 33A
0.90 PRE 40347
PRE 49411
(53-3128)
*
12.00
1
1
0.90 GROUP 32A
0.90 PRE 49411
(53-3128)
OR
GROUP 33A
POST 40347
12.00 PRE 49411
(53-3128)
OR
GROUP 33B
PRE 49411
(53-3128)
OR
GROUP 33C
PRE 49411
(53-3128)
OR
GROUP 33D
PRE 49411
(53-3128)
*
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR 13,
FROM STR 9 AFT TO STR 26, EXCLUDING 5 ROWS AT STR 9
FORWARD LEVEL, LH/RH.
* * * * *
1
1
ALI REFERENCE:
531186-01-02
PREP.: BOLTS;
DOOR FRAME LININGS Z220;
INSULATION Z220;
LAVATORIES Z220;
531186-01-3
MEN
1
1
0.50 GROUP 33A
0.50 PRE 40347
1
1
0.50 GROUP 32A
0.50 OR
GROUP 33A
ALI REFERENCE:
531188-01-02
ALI WFD
531100-200-868
4400 FC
ALI REFERENCE:
REV. DATE: JUL 01/21
SECTION:
* * * * *
3 -53
PAGE 28
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531188-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
531189-01-2
531188-01-03
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR 13,
FROM STR 9 AFT TO STR 26, EXCLUDING 5 ROWS AT STR 9
FORWARD LEVEL, LH/RH.
T: 33300 FC
221 MAIN STRUCTURE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FORWARD PAX / CREW DOOR CUT-OUT, FORWARD UPPER
LONGERON AT STR 12 LEVEL, BETWEEN FR 13A AND FR 13B,
LH/RH.
T: 29300 FC
I:
I:
ALI WFD
4400 FC
531100-200-868
531192-01-3
ALI
8800 FC
531100-200-854
ALI REFERENCE:
531189-01-02
APPLICABILITY
221 MAIN STRUCTURE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9
FORWARD, AND FR 13 AFT FACE STR 12, LH/RH.
1
1
0.50 GROUP 32E
0.50 PRE 53102
OR
GROUP 33E
PRE 53102
1
1
0.10 GROUP 32A
0.10 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
OR
6.00 GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
*
T: 21800 FC
I:
ALI
8100 FC
531100-200-842
1
1
ALI REFERENCE:
531192-01-03
PREP.: CREW REST ROOM IF INSTALLED;
GALLEYS (IF INSTALLED);
INSULATION TO BE DISPLACED AS REQUIRED;
LAVATORIES Z220;
LINING Z220;
STRUCTURE : FUSELAGE
M/H
POST 40347
OR
GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
ALI REFERENCE:
531188-01-03
PREP.: DOOR FRAME LININGS Z220;
INSULATION Z220;
R
MEN
* * * * *
CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR 13,
FROM STR 9 AFT TO STR 26, EXCLUDING 5 ROWS AT STR 9
FORWARD LEVEL, LH/RH.
531188-01-4
REFERENCE
*
REV. DATE: JUL 01/21
SECTION:
3-53
0.20 A330-200
0.20 OR
A330-200F
OR
A330-300
OR
22.00 A330-800
OR
A330-900
PRE 207735
PAGE 29
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
531193-01-1
R
531194-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
211 MAIN STRUCTURE
NDT SDI
212
SPECIAL DETAILED INSPECTION (HFEC & LFEC) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 7, ABOVE WINDOW FRAME,
LH/RH.
T: 40200 FC
221 MAIN STRUCTURE
AF
DET
222
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
STR 14 AND STR 22 BETWEEN FR 17 AND FR 18, LH/RH.
T: 21800 FC
I:
I:
SOURCE
ALI
5600 FC
REFERENCE
531100-250-831
ALI
8100 FC
531100-200-843
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF LONGITUDINAL
JUNCTION LATERAL PANELS AT STR 46, EXTERNAL SURFACE
BETWEEN FR 15A AND FR 18, LH/RH.
531198-01-2
121 MAIN STRUCTURE
AF
DET
122
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL
BETWEEN FR 13A AND FR 14, AND FR 16 AND FR 17, LH/RH.
T: 22000 FC
I: 13400 FC
T: 29300 FC
I:
531100-270-810
STRUCTURE : FUSELAGE
C O N T I N U E D
1
2.26 GROUP 32E
POST 55817
OR
GROUP 33E
POST 55817
ALI
8800 FC
531100-200-844
1
1
0.15 GROUP 32A
0.15 PRE 49194
OR
GROUP 33A
OR
GROUP 33B
TBD OR
GROUP 33C
PRE 49194
OR
GROUP 33D
PRE 49194
ALI REFERENCE:
531198-01-02
*
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 23 TO FR 25 AT STR 40 - STR 41 (LH).
* * * * *
0.10 A330-200
0.10 OR
A330-200F
OR
A330-300
6.00 OR
A330-800
OR
A330-900
PRE 207735
ALI REFERENCE:
531196-01-02
PREP.: INSULATION Z120;
532002-01-1
1
1
ALI REFERENCE:
531194-01-03
ALI
T: 21300 FC
I:
ALI WFD
532100-220-847
4800 FC
ALI REFERENCE:
532002-01-01
REV. DATE: JUL 01/21
SECTION:
APPLICABILITY
0.60 A330-200
0.60 OR
A330-300
*
100 MAIN STRUCTURE
M/H
1
1
ALI REFERENCE:
531193-01-01
PREP.: DOOR FRAME LININGS Z220;
INSULATION Z220;
531196-01-2
MEN
1
1
0.20 GROUP 33A
0.20 PRE 204516
(53-3248),
(53-3258)
* * * * *
3-53
PAGE 30
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532002-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 23 TO FR 25 AT STR 40 - STR 41 (LH).
T: 27700 FC
I:
ALI WFD
7200 FC
532100-220-847
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 23 TO FR 25 AT STR 40 - STR 41 (LH).
T: 21200 FC
I:
ALI WFD
3300 FC
532100-220-847
ALI REFERENCE:
532002-01-03
ACCESS: 821
532003-01-1
100 FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF SKIN AND BUTT
STRAP AT CIRCUMFERENTIAL JOINT FR 31 AT STR 27 TO STR
29, LH.
532004-01-1
STRUCTURE : FUSELAGE
*
0.10
1
1
0.20 GROUP 33B
0.20 PRE 45403
PRE 204516
(53-3248),
(53-3258)
*
0.10
1
1
0.20 GROUP 32A
0.20 PRE 45403
PRE 204516
(53-3248),
(53-3258)
*
0.10
1
1.80 A330-200F
1
1
0.25 GROUP 33A
0.25 PRE 204516
(53-3248)
ALI REFERENCE:
532002-01-02
ACCESS: 821
532002-01-3
M/H
APPLICABILITY
* * * * *
ACCESS: 821
532002-01-2
MEN
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 20 TO FR 22, BETWEEN STR 40 - STR 41 (LH).
T: 18300 FC
OR
57700 FH
I:
532100-220-856
ALI REFERENCE:
532003-01-01
2800 FC
OR
9000 FH
T: 21300 FC
I:
ALI
ALI WFD
4800 FC
532100-220-848
ALI REFERENCE:
532004-01-01
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
REV. DATE: JUL 01/21
SE CTION:
3-53
PAGE 31
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532004-01-2
532004-01-5
532009-01-1
R
532010-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 20 TO FR 22, BETWEEN STR 40 - STR 41 (LH).
T: 27700 FC
I:
SOURCE
ALI WFD
7200 FC
REFERENCE
532100-220-848
1
1
ALI REFERENCE:
532004-01-02
M/H
APPLICABILITY
0.25 GROUP 33B
0.25 PRE 45403
PRE 204516
(53-3248),
(53-3258)
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
1
1
0.25 GROUP 32A
0.25 PRE 45403
PRE 204516
(53-3248),
(53-3258)
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 20 TO FR 22, BETWEEN STR 40 - STR 41 (LH).
T: 21200 FC
I:
ALI WFD
3300 FC
532100-220-848
ALI REFERENCE:
532004-01-05
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC+US) OF FRAMES FROM
FR 37.1 TO FR 37.4, BETWEEN STR 38 AND STR 40 LH/RH.
T: 31500 FC
I:
ALI WFD
7200 FC
532100-220-851
1
1
ALI REFERENCE:
532009-01-01
PREP.: FLOOR PANELS Z130;
INSULATION Z130;
LINING Z130;
*
ACCESS: 821
*
134 FORWARD FUSELAGE
SPECIAL DETAILED INSPECTION (HFEC)
INTERNAL STRUCTURE BELOW FWD CARGO
FROM FR 20 TO FR 25 AND FROM CARGO
LEVEL TO STR 46 RH IN AREA OF LOCK
SHEARPLATES.
NDT
SDI
OF FUSELAGE
COMPARTMENT DOOR
COMPARTMENT FLOOR
FITTINGS AND
T: 25800 FC
I:
ALI WFD
4000 FC
532100-220-864
* * * * *
C O N T I N U E D
1
ALI REFERENCE:
532010-01-01
PREP.: FLOOR PANELS Z130;
STRUCTURE : FUSELAGE
MEN
*
0.60 GROUP 33A
0.60 POST 204516
(53-3248),
(53-3258)
OR
25.00 GROUP 33B
PRE 45405
POST 204516
(53-3248),
0.10 (53-3258)
1.40 A330-800
OR
A330-900
25.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 32
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532010-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.10
1
1.40 A330-200
OR
A330-300
OR
A330-200F
* * * * *
INSULATION Z130;
LINING Z130;
ACCESS: 821
N
532010-01-3
134 FORWARD FUSELAGE
SPECIAL DETAILED INSPECTION (HFEC)
INTERNAL STRUCTURE BELOW FWD CARGO
FROM FR 20 TO FR 25 AND FROM CARGO
LEVEL TO STR 46 RH IN AREA OF LOCK
SHEARPLATES.
NDT
SDI
OF FUSELAGE
COMPARTMENT DOOR
COMPARTMENT FLOOR
FITTINGS AND
PREP.: FLOOR PANELS Z130;
INSULATION Z130;
LINING Z130;
FH OPTIMIZED:
T: 25300 FC
OR
152300 FH
I:
I:
R
532015-02-1
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC+US) OF FRAMES FOR
A330-300 FROM FR 26.1 TO FR 37 AND FOR A330-200 FROM
FR 29 TO FR 37, BETWEEN STR 34 AND STR 35 LH/RH.
ALI REFERENCE:
532010-01-02
7600 FC
OR
45600 FH
25.00
*
0.10
1
1
2.00 A330-200
2.00 OR
A330-300
4000 FC
OR
12200 FH
T: 29300 FC
I:
*
ALI WFD
6900 FC
532100-220-852
ALI REFERENCE:
532015-01-01
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
1
1
2.00 A330-800
2.00 OR
A330-900
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC+US) OF FRAMES FOR
A330-900 FROM FR 26.1 TO FR 37 AND FOR A330-800 FROM
FR 29 TO FR 37, BETWEEN STR 34 AND STR 35 LH/RH.
* * * * *
STRUCTURE : FUSELAGE
532100-220-864
FC OPTIMIZED:
T: 38400 FC
OR
115400 FH
ACCESS: 821
532015-01-1
ALI WFD
C O N T I N U E D
T: 30300 FC
I:
ALI WFD
532100-220-887
6900 FC
ALI REFERENCE:
532015-02-01
REV. DATE: JUL 01/21
SECTION:
* * * * *
3 -53
PAGE 33
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532015-02-1
532016-01-1
532017-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
1
1
3.00 GROUP 33A
3.00 OR
GROUP 33B
PRE 45404
131 FORWARD FUSELAGE
NDT SDI
132
SPECIAL DETAILED INSPECTION (HFEC+US) OF FRAMES FROM
FR 26.1 TO FR 37 BETWEEN STR 39 AND STR 40 LH/RH.
T: 31400 FC
I:
ALI WFD
4800 FC
532100-220-859
ALI REFERENCE:
532016-01-01
PREP.: INSULATION Z130;
LINING Z130;
*
TBD
ACCESS: 821
*
0.10
1
1
0.10 A330-200
0.10 OR
A330-300
1
1
0.20 A330-200
0.20 OR
A330-300
1
0.08 A330-200F
243 FORWARD FUSELAGE
AF
GVI
244
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE AT FRAME FR 33, BETWEEN STR 7 AND STR 11
LH/RH.
T: 20800 FC
I:
ALI
2200 FC
532100-210-863
ALI REFERENCE:
532017-01-01
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532017-02-1
532017-02-1
243 FORWARD FUSELAGE
AF
DET
244
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AT FRAME FR 33, BETWEEN STR 7 AND STR 11 LH/RH.
T: 20800 FC
I:
ALI
6900 FC
532100-220-853
ALI REFERENCE:
532017-02-01
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532017-01-1
532018-01-1
200 FORWARD FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE AT FRAMES FR 23 AND FR 24, BETWEEN STR 7 AND
STR 10 RH.
T: 10400 FC
OR
31300 FH
I:
ALI
532100-210-864
ALI REFERENCE:
532018-01-01
1500 FC
NOTE:
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 34
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532018-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
THIS TASK IS AN ALTERNATIVE TO TASK 532018-02-1
532018-02-1
200 FORWARD FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AT FRAMES FR 23 AND FR 24, BETWEEN STR 7 AND STR 10
RH.
T: 10400 FC
OR
31300 FH
I:
ALI
532100-220-854
1
0.17 A330-200F
1
1
1
1
0.13
0.13
0.13
0.13
ALI REFERENCE:
532018-02-01
5300 FC
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532018-01-1
R
532021-01-1
532022-01-1
532023-01-1
131 FORWARD FUSELAGE
AF
DET
132
241 DETAILED INSPECTION OF DOOR 2 SURROUND FRAMES, FR 33
242 AND FR 35A, LH/RH.
T: 31000 FC
I:
ALI
8000 FC
532100-220-857
ALI REFERENCE:
532021-01-01
PREP.: INSULATION Z130;
INSULATION Z240;
LINING Z130;
LINING Z240;
*
ACCESS: 821
*
0.14
1
0.80 A330-200
OR
A330-300
1
1
0.18 GROUP 33A
0.18
832
842
100 FORWARD FUSELAGE
DET
T: 30300 FC
DETAILED INSPECTION OF SKIN AT STATIC PORT ATTACHMENT
HOLES
- FROM FR 30 TO FR 33 (FOR A330-200)
- FROM FR 26.2 TO FR 28 (FOR A330-300) BETWEEN STR 39
AND STR 40 AND BETWEEN STR 43 AND STR 44, LH/RH.
I: 15500 FC
133 FORWARD
134
SPECIAL
FITTING
BETWEEN
AF
FUSELAGE
NDT
SDI
DETAILED INSPECTION (HFEC) OF REINFORCEMENT
AT EXTRACTION AIR CUT OUT FROM FR 24 TO FR 25
STR 54 LH AND STR 54 RH.
T: 40000 FC
I:
ALI
532100-220-877
ALI REFERENCE:
532022-01-01
ALI
7500 FC
532100-220-878
ALI REFERENCE:
532023-01-01
PREP.: CARGO COMPARTMENT FLOOR PANELS Z130;
INSULATION Z130;
* * * * *
STRUCTURE : FUSELAGE
A330-200
OR
A330-300
OR
A330-800
3.00 OR
A330-900
PRE 207504
C O N T I N U E D
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 35
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532023-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.10
1
0.13 A330-200
OR
A330-300
1
0.50 A330-200
OR
A330-300
1
0.50 A330-200F
1
0.50 A330-800
OR
A330-900
* * * * *
LINING Z130;
ACCESS: 821
532024-01-1
200 FORWARD FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF SKIN BETWEEN FR 32 AND
FR 34, FROM STR 9 TO STR 13 LH/RH, EXTERNAL
STRUCTURE.
532101-01-2
100 MAIN STRUCTURE
AF
T: 29300 FC
ALI
I: 11200 FC
532100-210-865
ALI REFERENCE:
532024-01-01
GVI
T:
2200 FC
MRB
532100-210-801
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS,
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
2200 FC
GVI
T:
1500 FC
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
1500 FC
GVI
T:
3400 FC
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
3400 FC
MRB REFERENCE:
532101-01-5
REV. DATE: JUL 01/21
SECTION:
MRB REFERENCE:
532101-01-4
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-2.
532101-01-3
100 MAIN STRUCTURE
AF
MRB
532100-210-801
MRB REFERENCE:
532101-01-3
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-3.
N
532101-01-5
100 MAIN STRUCTURE
AF
MRB
532100-210-801
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-4
STRUCTURE : FUSELAGE
3-53
PAGE 36
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532101-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
100 MAIN STRUCTURE
AF
DET
T:
6900 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS,
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
6900 FC
DET
T:
5300 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
5300 FC
DET
T:
8400 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM
CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND
EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.
I:
8400 FC
T:
6 YE
I:
6 YE
SOURCE
MRB
REFERENCE
532100-220-827
MEN
M/H
APPLICABILITY
1
1.00 A330-200
OR
A330-300
1
1.00 A330-200F
1
1.00 A330-800
OR
A330-900
1
1
3.50 ALL
3.50
PREP.: CARGO COMPARTMENT FLOOR PANELS;
*
0.30
ACCESS: 821
*
0.10
MRB REFERENCE:
532101-02-2
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-2.
532101-02-3
100 MAIN STRUCTURE
AF
MRB
532100-220-827
MRB REFERENCE:
532101-02-3
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-3.
N
532101-02-4
100 MAIN STRUCTURE
AF
MRB
532100-220-827
MRB REFERENCE:
532101-02-4
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-5
532102-01-1
133 MAIN STRUCTURE
AF
134
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BETWEEN FR 20 AND FR 39.1 BELOW CARGO
COMPARTMENT FLOOR PANELS.
TPS
STRUCTURE : FUSELAGE
GVI
MRB CPCP
532100-210-821
MRB REFERENCE:
532102-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 37
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532104-01-1
ZONE
131 MAIN STRUCTURE
AF
DET
132
DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE
FROM MAIN DECK FLOOR TO CARGO COMPARTMENT FLOOR,
BELOW AND 0,75 M FWD AND AFT OF GALLEYS AND TOILETS,
FROM FR 20 TO FR 39.1, LH/RH.
TPS
532105-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
6 YE
532100-200-810
1
1
MRB REFERENCE:
532104-01-1
*
ACCESS: 821
*
134 MAIN STRUCTURE
AF
DET
6 YE
I:
6 YE
MRB CPCP
532100-200-801
APPLICABILITY
1.25 A330-200
1.25 GALLEYS/ TOILETS
INSTALLED FROM FR
20 TO FR 39.1 LH/RH
OR
A330-300
GALLEYS/ TOILETS
INSTALLED FROM FR
20 TO FR 39.1 LH/RH
OR
0.07 A330-800
GALLEYS/ TOILETS
INSTALLED FROM FR
0.10 20 TO FR 39.1 LH/RH
OR
A330-900
GALLEYS/ TOILETS
INSTALLED FROM FR
20 TO FR 39.1 LH/RH
1.20 ALL
PREP.: BALLMATS;
*
0.10
ACCESS: 821
*
0.10
1
0.25 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
532105-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
134 MAIN STRUCTURE
TPS
T:
M/H
1
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR
25 (10 PLACES).
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
* * * * *
STRUCTURE : FUSELAGE
I:
MRB CPCP
MEN
PREP.: CARGO COMPARTMENT LINING;
INSULATION TO BE DISPLACED AS REQUIRED;
TPS
532107-01-1
6 YE
REFERENCE
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BELOW FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN
FR 19 AND FR 26 FROM CARGO COMPARTMENT FLOOR TO STR
46 RH.
R
T:
SOURCE
C O N T I N U E D
T:
I:
6 YE
OR
3400 FC
MRB
MRB CPCP
6 YE
OR
3400 FC
532100-200-811
MRB REFERENCE:
532107-01-1
532107-01-2
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 38
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
*
0.10
1
0.25 A330-200F
*
0.10
1
0.50 ALL
*
0.10
*
0.10
1
1
0.50 ALL
0.50
PREP.: INSULATION;
LINING;
*
0.03
ACCESS: 821
*
0.10
1
1
0.10 A330-200F
0.10
532107-01-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
* * * * *
ACCESS: 821
532107-01-3
134 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR
25 (10 PLACES).
TPS
T:
I:
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
6 YE
OR
5000 FC
MRB
MRB CPCP
6 YE
OR
5000 FC
532100-200-811
MRB REFERENCE:
532107-01-1
532107-01-3
ACCESS: 821
532107-02-1
134 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO
COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND
FR 25.
PREP.: ECCENTRIC BOLTS;
ST:
6 YE
T:
24 YE
SI:
6 YE
I:
6 YE
MRB CPCP
532100-220-816
MRB REFERENCE:
532107-02-1
ACCESS: 821
532108-01-1
122 MAIN STRUCTURE
AF
DET
132
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN
FR 19 AND FR 26 FROM STR 26 RH TO CARGO COMPARTMENT
FLOOR LEVEL.
TPS
532114-01-6
T:
12 YE
I:
12 YE
MRB CPCP
532100-200-804
MRB REFERENCE:
532108-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
100 MAIN STRUCTURE
200
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
AF
C O N T I N U E D
DET
T: 17000 FC
MRB
532100-210-802
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 39
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
532114-01-6
* * * * *
C O N T I N U E
532115-01-1
132 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL
FRAMES (FR 20A AND FR 25A).
TPS
REFERENCE
I:
8000 FC
T:
6 YE
I:
6 YE
MRB CPCP
532100-200-812
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL
FRAMES (FR 20A AND FR 25A).
TPS
532115-02-1
T:
I:
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
132 FORWARD FUSELAGE
AF
DET
DETAILED INSPECTION OF LATERAL FRAMES OF FORWARD
CARGO COMPARTMENT DOOR CUTOUT, VISIBLE PART OF
LATERAL FRAMES (FR 20A AND FR 25A).
6 YE
OR
6600 FC
MRB
MRB CPCP
532100-200-812
STRUCTURE : FUSELAGE
*
0.10
1
0.20 A330-200F
*
0.10
1
0.17 A330-200
OR
A330-300
OR
A330-800
OR
0.10 A330-900
MRB REFERENCE:
532115-01-1
532115-01-3
6 YE
OR
6600 FC
T: 13300 FC
ALI
I: 13300 FC
532100-220-845
ALI REFERENCE:
532115-02-01
ACCESS: 821
532116-01-1
0.20 A330-200
OR
A330-300
OR
A330-800
OR
A330-900
MRB REFERENCE:
532115-01-1
ACCESS: 821
R
APPLICABILITY
1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
132 MAIN STRUCTURE
M/H
MRB REFERENCE:
532114-01-6
ACCESS: 821
532115-01-2
MEN
* * * * *
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AROUND FORWARD CARGO COMPARTMENT DOOR CUTOUT AT UPPER
AND LOWER CORNERS.
R
SOURCE
233 MAIN STRUCTURE
NDT SDI
234
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN
INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION
PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 6 AND CROWN
CENTERLINE, LH/RH.
*
T:
12 YE
I:
12 YE
MRB CPCP
REV. DATE: JUL 01/21
532100-220-801
MRB REFERENCE:
532116-01-1
SECTION:
3 -53
1
1
0.50 A330-300
0.50 PRE 42069
PRE 44826
PAGE 40
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532116-02-1
532116-03-1
532117-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
233 MAIN STRUCTURE
NDT SDI
234
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN
INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION
PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 13 AND CROWN
CENTERLINE, LH/RH.
T:
12 YE
I:
12 YE
233 MAIN STRUCTURE
NDT SDI
234
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN
INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION
PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 3 AND CROWN
CENTERLINE AND BETWEEN STR 7 TO STR 17, LH/RH.
T:
12 YE
I:
12 YE
200 MAIN STRUCTURE
T: 20000 FC
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26,
LH/RH.
I:
SOURCE
MRB CPCP
REFERENCE
532100-220-808
MEN
532100-220-809
0.50 A330-300
0.50 POST 42069
PRE 44826
1
1
0.50 A330-300
0.50 POST 44826
OR
A330-900
1
1.00 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
OR
GROUP
MRB REFERENCE:
532116-03-1
MRB
2200 FC
532100-210-803
MRB REFERENCE:
532117-01-6
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-3.
532117-01-4
200 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26,
LH/RH.
T: 17000 FC
I:
MRB
1500 FC
532100-210-803
APPLICABILITY
1
1
MRB REFERENCE:
532116-02-1
MRB CPCP
M/H
32A
33A
33B
33C
33D
1
1.00 A330-200F
1
1.00 GROUP 32E
OR
GROUP 33E
MRB REFERENCE:
532117-01-4
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-4.
532117-01-5
200 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26,
LH/RH.
T: 17000 FC
I:
MRB
532100-210-803
2200 FC
MRB REFERENCE:
532117-01-5
REV. DATE: JUL 01/21
SECTION:
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-5.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
3 -53
PAGE 41
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532117-01-5
N
532117-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
200 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26,
LH/RH.
T: 17000 FC
I:
MRB
3100 FC
532100-210-803
1
1.00 A330-800
OR
A330-900
1
2.00 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
OR
GROUP
MRB REFERENCE:
532117-01-7
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-5.
532117-02-3
200 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH.
T: 20000 FC
I:
MRB
6900 FC
532100-220-830
MRB REFERENCE:
532117-02-3
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-3.
532117-02-4
200 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH.
T: 17000 FC
I:
MRB
5300 FC
532100-220-830
32A
33A
33B
33C
33D
1
2.00 A330-200F
1
2.00 GROUP 32E
OR
GROUP 33E
1
2.00 A330-800
OR
MRB REFERENCE:
532117-02-4
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-4.
532117-02-5
200 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH.
T: 17000 FC
I:
MRB
6900 FC
532100-220-830
MRB REFERENCE:
532117-02-5
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-5.
N
532117-02-6
200 MAIN STRUCTURE
* * * * *
STRUCTURE : FUSELAGE
AF
C O N T I N U E D
DET
T: 17000 FC
MRB
532100-220-830
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 42
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
532117-02-6
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH.
I:
9500 FC
T:
6 YE
I:
6 YE
MRB REFERENCE:
532117-02-6
A330-900
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-7
532122-01-1
131 MAIN STRUCTURE
AF
DET
132
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT
BETWEEN FR 32 AND FR 36, FROM MAIN DECK FLOOR DOWN TO
STR 30, LH/RH.
1
1
0.50 A330-200
0.50 OR
A330-300
OR
A330-800
OR
A330-900
PREP.: AIR CONDITION DUCTS;
INSULATION TO BE DISPLACED AS REQUIRED;
SIDEWALL LINING;
*
0.50
ACCESS: 821
*
0.10
1
1
1
1
0.38
0.38
0.38
0.38
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
SIDEWALL/DOOR FRAME LINING;
*
TBD
ACCESS: 832
*
0.04
1
1.00 A330-200
OR
A330-300
OR
TPS
532123-01-1
532124-01-1
MRB REFERENCE:
532122-01-1
T:
12 YE
I:
12 YE
MRB CPCP
532100-200-808
MRB REFERENCE:
532123-01-1
A330-200
OR
A330-300
OR
A330-800
OR
A330-900
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
842
100 MAIN STRUCTURE
AF
DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW
DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE,
* * * * *
STRUCTURE : FUSELAGE
532100-200-802
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
241 MAIN STRUCTURE
AF
DET
242
243 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
244 AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUTOUT
BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOOR UP TO
STR 9, LH/RH.
TPS
MRB CPCP
C O N T I N U E D
DET
T:
12 YE
I:
6 YE
MRB CPCP
532100-200-809
MRB REFERENCE:
532124-01-1
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 43
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532124-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
532124-02-4
532124-02-5
532124-02-6
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
A330-800
OR
4.00 A330-900
ACCESS: 832
*
0.04
1
1
5.00 GROUP 32E
5.00 PRE 204658
(53-3264)
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
1
1
2.50 GROUP 32A
2.50 PRE 204658
(53-3264)
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
1
1
2.50 GROUP 33A
2.50 PRE 45293
(53-3086)
PRE 204658
(53-3264)
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
1
1
2.50 GROUP 33A
2.50 POST 45293
(53-3086)
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
T: 10200 FC
I:
ALI
3700 FC
532100-220-802
ALI REFERENCE:
532124-02-10
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
T: 10400 FC
I:
ALI
3500 FC
532100-220-802
ALI REFERENCE:
532124-02-04
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
T: 17100 FC
I:
ALI
3400 FC
532100-220-802
ALI REFERENCE:
532124-02-05
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
* * * * *
LH/RH.
532124-02-1
M/H
C O N T I N U E D
T: 16200 FC
I:
ALI
532100-220-802
4800 FC
ALI REFERENCE:
REV. DATE: JUL 01/21
SECTION:
* * * * *
3-53
PAGE 44
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532124-02-6
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
1
1
2.50 GROUP 33B
2.50 PRE 204658
(53-3264)
OR
GROUP 33C
PRE 204658
4.00 (53-3264)
OR
0.04 GROUP 33D
PRE 204658
(53-3264)
* * * * *
C O N T I N U E
SOURCE
532124-02-9
532124-02-11
532124-02-06
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
T: 10200 FC
I:
ALI
3400 FC
532100-220-802
ALI REFERENCE:
532124-02-08
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
ACCESS: 832
*
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
1
1
5.00 GROUP 33E
5.00 PRE 204658
(53-3264)
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
T: 11200 FC
1
1
5.00 GROUP 33B
5.00 POST 204658
(53-3264)
OR
GROUP 33C
POST 204658
4.00 (53-3264)
OR
0.04 GROUP 33D
POST 204658
(53-3264)
I:
ALI
3600 FC
532100-220-802
ALI REFERENCE:
532124-02-09
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
T: 31600 FC
I:
ALI
3400 FC
532100-220-802
ALI REFERENCE:
532124-02-11
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
ACCESS: 832
*
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
* * * * *
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
532124-02-8
REFERENCE
842
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 45
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532124-02-11
R
532124-02-12
532124-03-1
532125-01-5
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR 2 (MID
PASSENGER / CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
MEN
M/H
APPLICABILITY
1
1
5.00 A330-800
5.00 OR
A330-900
PREP.: SCUFF PLATES BELOW Z832/Z842;
*
4.00
ACCESS: 832
*
0.04
1
1
2.80 GROUP 33A
2.80 POST 45293
(53-3086)
PREP.: SCUFF PLATE;
*
0.30
ACCESS: 832
*
0.04
1
5.00 GROUP 33A
PRE 45293
(53-3086)
PRE 204658
*
0.04
1
4.00 GROUP
OR
GROUP
OR
GROUP
OR
0.04 GROUP
I:
ALI
5600 FC
532100-220-802
ALI REFERENCE:
532124-02-12
T: 16200 FC
ALI
I: 12600 FC
532100-220-850
ALI REFERENCE:
532124-03-01
842
200 MAIN STRUCTURE
NDT
SDI
T:
3400 FC
I:
3400 FC
ALI
532100-220-803
ALI REFERENCE:
532125-01-05
842
200 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER
CORNERS.
ACCESS: 832
T: 14400 FC
842
100 MAIN STRUCTURE
NDT SDI
200
SPECIAL DETAILED INSPECTION (ROTOTEST) OF DOOR 2 (MID
PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH
SCUFF PLATE, LH/RH.
ACCESS: 832
STRUCTURE : FUSELAGE
REFERENCE
* * * * *
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER
CORNERS.
532125-01-8
SOURCE
T:
3400 FC
I:
3400 FC
ALI
532100-220-803
ALI REFERENCE:
532125-01-08
842
*
REV. DATE: JUL 01/21
SECTION:
3 -53
32A
33B
33C
33D
PAGE 46
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532125-01-9
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER
CORNERS.
ACCESS: 832
R
532125-01-11
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
AT DOOR 2 (MID PASSENGER / CREW DOOR) CUT-OUT
STRUCTURE UPPER CORNER LH/RH.
532125-02-1
3600 FC
I:
3600 FC
ALI
REFERENCE
532100-220-803
T:
5700 FC
I:
5700 FC
ALI
532100-220-803
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
SKIN AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT
UPPER CORNERS.
T: 10900 FC
ALI
I: 10900 FC
532100-220-886
ACCESS: 832
532125-03-6
200 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE SKIN AT
DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER
CORNERS.
ACCESS: 832
532126-01-1
T:
4300 FC
I:
4300 FC
ALI
532100-220-863
1
0.67 A330-800
OR
A330-900
*
0.04
1
T: 26100 FC
ALI
I: 18100 FC
532100-210-841
ALI REFERENCE:
532126-01-01
C O N T I N U E D
10.12 GROUP 33A
POST 45293
(53-3086)
OR
GROUP 33A
POST 204658
TBD
*
0.04
1
1.13 GROUP 33A
POST 45293
(53-3086)
OR
GROUP 33A
POST 204658
0.04
*
PREP.: DOOR FRAME LININGS Z240;
STRUCTURE : FUSELAGE
0.04
ALI REFERENCE:
532125-01-06
842
243 MAIN STRUCTURE
AF
DET
244
DETAILED INSPECTION OF DOOR 2, COVER PLATE OF TORSION
BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND STR 13
LH/RH.
* * * * *
*
*
842
APPLICABILITY
4.00 GROUP 32E
OR
GROUP 33E
ALI REFERENCE:
532125-02-01
PREP.: BOLTS;
M/H
1
ALI REFERENCE:
532125-01-11
842
200 MAIN STRUCTURE
MEN
ALI REFERENCE:
532125-01-09
842
200 MAIN STRUCTURE
ACCESS: 832
T:
SOURCE
1
1
0.15 A330-200
0.15 OR
A330-300
*
3.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 47
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532126-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
*
0.04
1
1
0.15 A330-800
0.15 OR
A330-900
PREP.: DOOR FRAME LININGS Z240;
INSULATION Z240;
*
3.00
ACCESS: 832
*
0.04
1
3.07 A330-200
OR
A330-300
1
3.07 A330-800
OR
A330-900
1
1
1
1
1.00
1.00
1.00
1.00
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
INSULATION Z240;
ACCESS: 832
R
532126-01-2
532130-01-2
R
532130-01-5
532134-01-1
842
243 MAIN STRUCTURE
AF
DET
244
DETAILED INSPECTION OF DOOR 2, COVER PLATE OF TORSION
BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND STR 13
LH/RH.
T: 27600 FC
ALI
I: 15300 FC
532100-210-841
ALI REFERENCE:
532126-01-02
842
200 MAIN STRUCTURE
AF
DET
T: 20400 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR 18
AND FR 31, BETWEEN FR 36 AND FR 38, FROM STR 18 TO
STR 22, LH/RH.
I: 10000 FC
200 MAIN STRUCTURE
AF
DET
T: 29100 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR 18
AND FR 31, BETWEEN FR 36 AND FR 38, FROM STR 18 TO
STR 22, LH/RH.
I: 10900 FC
231 MAIN STRUCTURE
AF
DET
232
241 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE
242 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING
DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.
T:
5 YE
I:
5 YE
ALI
532100-210-824
ALI REFERENCE:
532130-01-02
ALI
532100-210-824
ALI REFERENCE:
532130-01-05
MRB CPCP
532100-200-803
MRB REFERENCE:
532134-01-1
NOTE:
- TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7
OF MPD STRUCTURE SECTION ARE NOT INCORPORATED
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
A330-200
GALLEYS/TOILETS
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION NOT
INCORPORATED
OR
A330-300
GALLEYS/TOILETS
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 48
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
532134-01-1
* * * * *
TPS
532134-02-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
SOURCE
REFERENCE
MEN
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
*
ACCESS: 831
*
841
231 MAIN STRUCTURE
AF
DET
232
241 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE
242 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING
DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.
T:
6 YE
I:
6 YE
MRB CPCP
532100-210-851
MRB REFERENCE:
532134-01-2
1
1
1
1
NOTE:
- TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7
OF MPD STRUCTURE SECTION ARE INCORPORATED
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FLOOR PANELS;
GALLEYS;
TOILETS;
*
ACCESS: 831
*
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
* * * * *
PREP.: FLOOR PANELS;
GALLEYS;
TOILETS;
TPS
M/H
841
C O N T I N U E D
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION NOT
INCORPORATED
10.30 OR
A330-800
GALLEYS/TOILETS
INSTALLED FROM FR
0.04 17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION NOT
INCORPORATED
OR
A330-900
GALLEYS/TOILETS
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION NOT
INCORPORATED
1.00
1.00
1.00
1.00
A330-200
GALLEYS/ TOILETS
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION
INCORPORATED
OR
A330-300
GALLEYS/ TOILETS
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION
INCORPORATED
10.30 OR
A330-800
GALLEYS/ TOILETS
INSTALLED FROM FR
0.04 17 TO FR 36 AND
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 49
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532134-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
NOTE 7 STRUCTURE
SECTION
INCORPORATED
OR
A330-900
GALLEYS/ TOILETS
INSTALLED FROM FR
17 TO FR 36 AND
NOTE 7 STRUCTURE
SECTION
INCORPORATED
532136-01-1
532139-01-1
233 MAIN STRUCTURE
NDT SDI
234
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
INTERNAL SKIN UNDERNEATH ACOUSTIC INSULATION PANELS
FROM FR 18 TO FR 32, BETWEEN STR 3 AND CROWN
CENTERLINE, LH/RH AND BETWEEN STR 7 TO STR 17, LH/RH.
T:
12 YE
I:
12 YE
100 MAIN STRUCTURE
T: 24600 FC
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AT CLOSED DRAIN MAST CUT-OUT BETWEEN FR 28 AND FR 29,
FROM STR 46 TO STR 47, RH.
532143-01-3
200 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF SKIN AROUND GPS ANTENNA
CUT-OUTS BETWEEN FR 35 AND FR 36 AND FR 37 AND FR
37.1, ON CROWN CENTERLINE, EXTERNAL SURFACE.
I:
532100-200-814
MRB REFERENCE:
532136-01-1
ALI
7700 FC
T: 17000 FC
I:
MRB CPCP
532100-210-844
532149-01-4
231 MAIN STRUCTURE
NDT SDI
232
233 SPECIAL DETAILED INSPECTION (LFEC & US) OF SPLICE
234 PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR 26, FROM
STR 4 TO STR 6, STR 12 TO STR 14 AND STR 21 TO STR
22, LH/RH.
MRB
5400 FC
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 25700 FC
OR
174300 FH
I:
1.50 A330-200
1.50 OR
A330-800
1
0.05 GROUP 33A
IF CUT OUT IN SKIN
EMBODIED
1
0.10 A330-200F
*
0.90
1
1
1
1
1.13 GROUP 33A
1.13 OR
1.13 GROUP 33B
1.13
ALI REFERENCE:
532139-01-01
532100-210-827
MRB REFERENCE:
532143-01-3
PREP.: GPS ANTENNAS;
R
1
1
ALI
532100-220-810
ALI REFERENCE:
532149-01-04
4900 FC
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 50
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532149-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
R
532149-01-5
FC OPTIMIZED:
T: 29800 FC
OR
89700 FH
842
I:
231 MAIN STRUCTURE
NDT SDI
232
233 SPECIAL DETAILED INSPECTION (LFEC & US) OF SPLICE
234 PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR 26, FROM
STR 4 TO STR 6, STR 12 TO STR 14 AND STR 21 TO STR
22, LH/RH.
PREP.: CEILING PANELS Z230;
INSULATION Z230;
OVERHEAD STOWAGE BINS Z230;
SIDEWALL PANELS Z230;
ACCESS: 832
R
532149-01-6
842
842
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF EXTERNAL SKIN
OF LONGITUDINAL LAP JOINT AT STR 22 (LH/RH), BETWEEN
STRUCTURE : FUSELAGE
MEN
M/H
APPLICABILITY
*
15.80
*
0.04
532100-220-810
1
1
1
1
1.13 GROUP 33C
1.13 OR
1.13 GROUP 33D
1.13
ALI REFERENCE:
532149-01-05
4800 FC
4800 FC
FH OPTIMIZED:
T: 30100 FC
OR
204200 FH
I:
I:
NDT
C O N T I N U E D
I:
ALI
ALI
532100-220-810
ALI REFERENCE:
532149-01-06
*
15.80
*
0.04
1
1
1
1
1.13 GROUP 32A
1.13
1.13
1.13
5200 FC
FC OPTIMIZED:
T: 34500 FC
OR
120800 FH
200 MAIN STRUCTURE
* * * * *
FH OPTIMIZED:
T: 27900 FC
OR
189600 FH
I:
PREP.: CEILING PANELS Z230;
INSULATION Z230;
OVERHEAD STOWAGE BINS Z230;
SIDEWALL PANELS Z230;
532151-01-1
4900 FC
FC OPTIMIZED:
T: 32800 FC
OR
98700 FH
231 MAIN STRUCTURE
NDT SDI
232
233 SPECIAL DETAILED INSPECTION (LFEC & US) OF SPLICE
234 PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR 26, FROM
STR 4 TO STR 6, STR 12 TO STR 14 AND STR 21 TO STR
22, LH/RH.
ACCESS: 832
REFERENCE
* * * * *
PREP.: CEILING PANELS Z230;
INSULATION Z230;
OVERHEAD STOWAGE BINS Z230;
SIDEWALL PANELS Z230;
ACCESS: 832
SOURCE
5200 FC
T: 31100 FC
ALI WFD
I: 11000 FC
532100-220-817
ALI REFERENCE:
532151-01-01
*
15.80
*
0.04
1
2.20 GROUP 33A
OR
GROUP 33B
PRE 45226
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 51
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532151-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FR 37.1 AND FR 38.
532153-01-2
100 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
OUTFLOW VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32
AND FR 33, FROM STR 45 TO STR 49, LH ONLY.
532154-01-2
200 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
AT SPOT LIGHT CUT-OUT, BETWEEN
- FR 27 AND FR 28 AND BETWEEN
- FR 29 AND FR 31,
- FROM STR 24 TO STR 26, LH/RH.
532155-01-2
100 MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AND DOUBLER AT
PRESSURE RELIEF VALVE CUT-OUT, BETWEEN FR 24 AND FR
25, FROM STR 26 TO STR 30, LH ONLY.
532164-01-1
132 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FWD FUSELAGE,
CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR 22 AND FR
23.
532166-01-3
I:
8000 FC
T: 29700 FC
I:
ALI
ALI
I:
0.10 A330-200
OR
A330-300
532100-210-833
1
0.10 A330-200
OR
A330-300
1
0.05 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
OR
GROUP
ALI REFERENCE:
532154-01-02
ALI
I: 11800 FC
T: 20300 FC
1
ALI REFERENCE:
532153-01-02
8500 FC
T: 36700 FC
532100-220-804
532100-210-834
ALI REFERENCE:
532155-01-02
MRB
6200 FC
532100-220-814
1
MRB REFERENCE:
532164-01-2
32A
33A
33B
33C
33D
0.25 GROUP 33B
POST 44072
PRE 45489
(53-3060)
PREP.: CEILING PANELS;
*
TBD
ACCESS: 821
*
0.10
1
0.30 A330-200
OR
200 MAIN STRUCTURE
* * * * *
STRUCTURE : FUSELAGE
T: 15200 FC
AF
C O N T I N U E D
GVI
T:
4500 FC
MRB
532100-210-853
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 52
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532166-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO
CROWN CENTERLINE.
I:
4500 FC
MRB REFERENCE:
532166-01-3
T:
6100 FC
I:
6100 FC
T:
7600 FC
I:
7600 FC
DET
T:
6900 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO CROWN
CENTERLINE.
I:
6900 FC
DET
T:
8100 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO CROWN
CENTERLINE.
I:
8100 FC
MRB REFERENCE:
532166-02-4
REV. DATE: JUL 01/21
SECTION:
A330-300
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-3.
532166-01-4
200 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO
CROWN CENTERLINE.
MRB
532100-210-853
1
0.30 A330-200F
1
0.30 A330-800
OR
A330-900
1
0.60 A330-200
OR
A330-300
1
0.60 A330-200F
MRB REFERENCE:
532166-01-4
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-4.
N
532166-01-5
200 MAIN STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL
SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO
CROWN CENTERLINE.
MRB
532100-210-853
MRB REFERENCE:
532166-01-5
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-5
532166-02-3
200 MAIN STRUCTURE
AF
MRB
532100-220-829
MRB REFERENCE:
532166-02-3
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-3.
532166-02-4
200 MAIN STRUCTURE
* * * * *
STRUCTURE : FUSELAGE
AF
C O N T I N U E D
MRB
532100-220-829
* * * * *
3 -53
PAGE 53
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
532166-02-4
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-4.
N
532166-02-5
200 MAIN STRUCTURE
AF
DET
T: 10400 FC
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE
BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO CROWN
CENTERLINE.
I: 10400 FC
MRB
532100-220-829
1
0.60 A330-800
OR
A330-900
1
1
1.75 A330-200F
1.75
MRB REFERENCE:
532166-02-5
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-5
532168-01-1
230 MAIN STRUCTURE
AF
GVI
240
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE FROM BARRIER WALL (BETWEEN FR 19 AND FR 20)
TO FR 36, FROM CROWN CENTERLINE TO MAIN DECK FLOOR,
LH/RH.
T:
12 YE
I:
12 YE
MRB CPCP
532100-210-857
MRB REFERENCE:
532168-01-1
NOTE:
TPS APPLICATION IN THE AREA BELOW STR 25.
TPS
: TYPE 3 TPS IS TO BE APPLIED.
PREP.: INSULATION Z230;
INSULATION Z240;
SIDEWALL LININGS Z230;
SIDEWALL LININGS Z240;
532169-01-1
*
230 MAIN STRUCTURE
AF
DET
240
DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE FROM
BARRIER WALL (BETWEEN FR 19 AND FR 20) TO FR 36.
TPS
T:
6 YE
I:
6 YE
MRB CPCP
532100-220-835
MRB REFERENCE:
532169-01-1
2.50 A330-200F
2.50
: TYPE 3 TPS IS TO BE APPLIED.
PREP.: CARGO LOADING SYSTEM Z230;
CARGO LOADING SYSTEM Z240;
FLOOR PANELS Z230;
* * * * *
STRUCTURE : FUSELAGE
1
1
20.00
C O N T I N U E D
*
69.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 54
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
532169-01-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FLOOR PANELS Z240;
532170-02-1
230 FORWARD FUSELAGE
AF
DET
DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO
FUSELAGE, FITTING ASSEMBLIES.
TPS
T:
12 YE
I:
12 YE
MRB CPCP
532100-220-834
: TYPE 3 TPS IS TO BE APPLIED.
230 FORWARD FUSELAGE
*
AF
DET
DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO
CARGO FLOOR, FITTING ASSEMBLIES.
TPS
T:
6 YE
I:
6 YE
MRB CPCP
532100-220-836
*
AF
GVI
GENERAL VISUAL INSPECTION OF BARRIER WALL FRAMES AND
BOX STRUCTURE.
T:
6 YE
I:
6 YE
MRB CPCP
532100-210-860
STRUCTURE : FUSELAGE
1
TBD
0.50 A330-200F
MRB REFERENCE:
532172-01-1
: TYPE 3 TPS IS TO BE APPLIED.
PREP.: BARRIER WALL LINING;
STOWAGE BINS (IF FITTED);
532175-02-2
0.75 A330-200F
: TYPE 3 TPS IS TO BE APPLIED.
230 FORWARD FUSELAGE
TPS
1
TBD
MRB REFERENCE:
532171-02-1
PREP.: BARRIER WALL LINING;
PROTECTION ANGLES AND DOOR STEPS;
532172-01-1
1.00 A330-200F
MRB REFERENCE:
532170-02-1
PREP.: BARRIER WALL LINING;
SMOKE CURTAIN;
STOWAGE BINS (IF FITTED);
532171-02-1
1
100 FORWARD FUSELAGE
AF
DET
200
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE
AROUND MAIN DECK CARGO DOOR CUT-OUT FROM FR 18 TO FR
31 AND FROM CROWN CENTERLINE TO STR 35.
*
T:
8000 FC
MRB
532100-220-866
I:
8000 FC
MRB REFERENCE:
532175-02-1
REV. DATE: JUL 01/21
SECTION:
3 -53
1
1
TBD
2.33 A330-200F
2.33
PAGE 55
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532177-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
231 FORWARD FUSELAGE
GVI
T:
6 YE
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
STRUCTURE OF MAIN DECK CARGO DOOR LOCK FITTING
ATTACHMENTS, SURROUNDING STRUCTURE AND LOWER LONGERON
FROM FR 20 TO FR 29 AND FROM STR 26 TO STR 30.
I:
6 YE
TPS
AF
SOURCE
MRB CPCP
REFERENCE
532100-210-859
*
231 FORWARD FUSELAGE
GVI
T:
4700 FC
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
STRUCTURE OF MAIN DECK CARGO DOOR LOCK FITTINGS FROM
FR 20 TO FR 29 AND FROM STR 26 TO STR 30 AT 8 PLACES.
I:
4700 FC
AF
231 FORWARD FUSELAGE
DET
T:
6 YE
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE OF
MAIN DECK CARGO DOOR LOCK FITTINGS FROM FR 20 TO FR
29 AND FROM STR 26 TO STR 30 AT 8 PLACES.
I:
6 YE
TPS
ALI
MRB
AF
MRB CPCP
532100-210-862
MRB REFERENCE:
532178-01-1
*
532100-220-837
1
AF
GVI
T:
I:
: TYPE 3 TPS IS TO BE APPLIED.
6 YE
OR
5200 FC
MRB
MRB CPCP
6 YE
OR
5200 FC
532100-210-855
TBD
0.20 A330-200F
*
230 FORWARD FUSELAGE
* * * * *
C O N T I N U E D
1
AF
GVI
T:
12 YE
MRB CPCP
TBD
0.30 A330-200F
MRB REFERENCE:
532179-01-1
532179-01-2
PREP.: MDC DOOR;
STRUCTURE : FUSELAGE
0.10 A330-200F
MRB REFERENCE:
532178-02-1
*
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE OF MAIN DECK CARGO DOOR CUT-OUT FR 20 AND
FR 29 FROM STR 5 TO STR 28.
532180-01-1
1
TBD
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
230 FORWARD FUSELAGE
TPS
0.10 A330-200F
ALI REFERENCE:
532178-01-01
PREP.: MDC DOOR;
532179-01-1
APPLICABILITY
: TYPE 3 TPS IS TO BE APPLIED.
PREP.: MDC DOOR;
532178-02-1
1
M/H
MRB REFERENCE:
532177-01-1
PREP.: MDC DOOR;
532178-01-1
MEN
532100-210-856
1
TBD
0.40 A330-200F
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 56
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
532180-01-1
* * * * *
C O N T I N U E
REFERENCE
I:
12 YE
T:
6 YE
I:
6 YE
MRB CPCP
532100-210-861
532184-01-1
233 FORWARD FUSELAGE
NDT SDI
234
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
SKIN AND CIRCUMFERENTIAL SPLICE AT FR 31 BETWEEN STR
6 AND CROWN CENTER LINE, LH/RH.
T: 10300 FC
OR
31000 FH
100 FORWARD FUSELAGE
T: 33000 FC
NDT
SDI
100 FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF LONGITUDINAL
BUTT JOINT BETWEEN FR 18 AND FR 20A AT STR 28 RH &
* * * * *
STRUCTURE : FUSELAGE
2.00
1
1
0.50 A330-200F
0.50
*
5.00
1
1
0.50 A330-200F
0.50 PRE 204501
(53-3244)
1
8.37 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
: TYPE 3 TPS IS TO BE APPLIED.
SPECIAL DETAILED INSPECTION (LFEC) OF LONGITUDINAL
BUTT JOINT BETWEEN FR 18 AND FR 20A AT STR 28 RH &
STR 39 RH.
532184-01-2
*
MRB REFERENCE:
532181-01-1
PREP.: INSULATION Z130;
SIDEWALL LININGS Z130;
532183-01-1
APPLICABILITY
: TYPE 3 TPS IS TO BE APPLIED.
121 FORWARD FUSELAGE
AF
GVI
131
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BELOW MAIN DECK CARGO DOOR CUT-OUT FROM FR
18 TO FR 31 AND FROM STR 26 TO STR 35.
TPS
M/H
MRB REFERENCE:
532180-01-1
PREP.: SIDEWALL LININGS Z230;
532181-01-1
MEN
* * * * *
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE AROUND MAIN DECK CARGO DOOR CUT-OUT FROM FR
18 TO FR 31 AND FROM CROWN CENTERLINE TO STR 26.
TPS
SOURCE
C O N T I N U E D
I:
ALI WFD
ALI REFERENCE:
532183-01-01
7300 FC
OR
21900 FH
ALI
I: 12100 FC
T: 35500 FC
532100-220-838
532100-220-839
ALI REFERENCE:
532184-01-01
ALI
I: 12100 FC
532100-220-839
1
33A
33B
33C
33D
8.37 GROUP 32A
ALI REFERENCE:
532184-01-02
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 57
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532184-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
STR 39 RH.
532185-01-1
231 FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS FROM FR 20 TO FR 25, BETWEEN STR 20
AND STR 23 RH.
532185-01-2
I:
ALI WFD
4300 FC
532100-220-840
ALI REFERENCE:
532185-01-01
1.75 GROUP 33A
PRE 204307
(53-3223)
*
15.00
ACCESS: 832
*
0.04
842
231 FORWARD FUSELAGE
NDT
SDI
T: 20600 FC
I:
ALI WFD
3500 FC
532100-220-840
1
ALI REFERENCE:
532185-01-02
PREP.: INSULATION Z230;
LINING Z230;
*
ACCESS: 832
*
842
231 FORWARD FUSELAGE
NDT SDI
232
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 26 TO FR 37.4 AT STR 40 - STR 41, LH/RH.
T: 21300 FC
I:
ALI WFD
4800 FC
532100-220-841
ALI REFERENCE:
532186-01-01
PREP.: INSULATION Z230;
* * * * *
STRUCTURE : FUSELAGE
1
PREP.: INSULATION Z230;
LINING Z230;
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS FROM FR 20 TO FR 25, BETWEEN STR 20
AND STR 23 RH.
532186-01-1
T: 33100 FC
C O N T I N U E D
1
1
*
1.75 A330-200
PRE 204307
(53-3223)
OR
GROUP 33B
PRE 204307
15.00 (53-3223)
OR
GROUP 33C
0.04 PRE 204307
(53-3223)
OR
GROUP 33D
PRE 204307
(53-3223)
OR
GROUP 33E
PRE 204307
(53-3223)
1.75 GROUP 33A
1.75 PRE 204516
(53-3248),
(53-3258)
15.00
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 58
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532186-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
*
0.10
APPLICABILITY
* * * * *
LINING Z230;
ACCESS: 821
532186-01-2
532189-01-1
R
532189-01-2
STRUCTURE : FUSELAGE
231 FORWARD FUSELAGE
NDT SDI
232
SPECIAL DETAILED INSPECTION (HFEC & US) OF FRAMES AND
FRAME COUPLINGS AT CARGO FLOOR ATTACHMENT FITTINGS
FROM FR 26 TO FR 37.4 AT STR 40 - STR 41, LH/RH.
T: 27700 FC
I:
ALI WFD
7200 FC
532100-220-841
1
1
ALI REFERENCE:
532186-01-02
PREP.: INSULATION Z230;
LINING Z230;
*
ACCESS: 821
*
231 FORWARD FUSELAGE
NDT SDI
232
SPECIAL DETAILED INSPECTION (ROTOTEST) OF DOOR 2, FR
33, BETWEEN STR 14 AND 15, LH / RH.
T:
5300 FC
I:
3800 FC
ALI
532100-220-843
ALI REFERENCE:
532189-01-01
1
1
PREP.: BOLTS;
INSULATION Z230;
LINING Z230;
*
ACCESS: 832
*
842
231 FORWARD FUSELAGE
NDT SDI
232
SPECIAL DETAILED INSPECTION (ROTOTEST) OF DOOR 2, FR
33, BETWEEN STR 14 AND 15, LH / RH.
T: 27100 FC
I:
ALI
6600 FC
532100-220-843
1
1
ALI REFERENCE:
532189-01-02
PREP.: BOLTS;
INSULATION Z230;
LINING Z230;
*
ACCESS: 832
*
842
REV. DATE: JUL 01/21
SECTION:
3 -53
1.75 GROUP 33B
1.75 PRE 45403
PRE 45404
PRE 45405
PRE 204516
(53-3248),
15.00 (53-3258)
0.10
1.00 GROUP 33A
1.00 PRE 44147
(53-3065)
OR
GROUP 33B
15.00 PRE 44147
(53-3065)
0.04
1.00 A330-200
1.00 OR
GROUP 33C
OR
GROUP 33D
15.00 OR
GROUP 33E
OR
A330-800
0.04 OR
A330-900
PRE 207504
PAGE 59
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532189-02-1
532191-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
231 FORWARD FUSELAGE
NDT SDI
232
SPECIAL DETAILED INSPECTION (HFEC & ROTO) OF DOOR 2,
FR 33, BETWEEN STR 14 AND 15, LH / RH.
532195-01-1
1
1
ALI REFERENCE:
532189-02-01
*
*
130 FORWARD FUSELAGE
NDT
200 FORWARD FUSELAGE
NDT
200 FORWARD FUSELAGE
NDT
SDI
SDI
SDI
233 FORWARD FUSELAGE
NDT SDI
234
SPECIAL DETAILED INSPECTION (HFEC & US) OF STRINGER
AND STRINGER COUPLING AT FR 26, STR 5 (LH/RH).
NOTE:
ROTO TEST INSPECTION TO BE PERFORMED IN CASE US
INSPECTION IS NOT FEASIBLE ACCORDING TO NTM.
* * * * *
STRUCTURE : FUSELAGE
5300 FC
532100-220-885
ACCESS: 832
842
SPECIAL DETAILED INSPECTION (LFEC) OF LOWER SKIN OF
LONGITUDINAL LAP JOINT AT STR 22 (LH/RH), BETWEEN FR
37.1 AND FR 38.
R
I:
ALI
MEN
*
SPECIAL DETAILED INSPECTION (LFEC) OF LOWER SKIN OF
LONGITUDINAL LAP JOINT AT STR 22 (LH/RH), BETWEEN FR
37.1 AND FR 38.
532192-01-2
5300 FC
REFERENCE
PREP.: BOLTS;
INSULATION Z230;
LINING Z230;
SPECIAL DETAILED INSPECTION (LFEC) OF UPPER SKIN OF
LONGITUDINAL LAP JOINT AT STR 31 (LH/RH), BETWEEN FR
31 AND FR 37.1.
532192-01-1
T:
SOURCE
C O N T I N U E D
T: 42200 FC
I:
ALI WFD
6800 FC
T: 33400 FC
ALI WFD
532100-220-865
APPLICABILITY
0.20 GROUP 33A
0.20 POST 44147
(53-3065)
OR
GROUP 33B
15.00 POST 44147
(53-3065)
0.02
0.02
10.13 GROUP
OR
GROUP
OR
GROUP
OR
GROUP
33B
33C
33D
33E
1
5.40 GROUP 33A
1
5.40 GROUP 33B
PRE 45226
1
1
0.27 GROUP 33A
0.27 OR
GROUP 33C
OR
GROUP 33D
ALI REFERENCE:
532192-01-01
ALI WFD
I: 11900 FC
FH OPTIMIZED:
T: 34700 FC
OR
234600 FH
1
ALI REFERENCE:
532191-01-02
I: 11000 FC
T: 31100 FC
532100-220-880
M/H
532100-220-865
ALI REFERENCE:
532192-01-02
ALI
532100-220-855
ALI REFERENCE:
532195-01-01
I: 14100 FC
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 60
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
532195-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
R
532195-01-2
REFERENCE
MEN
M/H
APPLICABILITY
*
15.00
*
0.04
1
1
0.27 GROUP 33B
0.27
* * * * *
PREP.: INSULATION Z230;
LINING Z230;
OVERHEAD STOWAGE BINS Z230;
ACCESS: 831
SOURCE
841
233 FORWARD FUSELAGE
NDT SDI
234
SPECIAL DETAILED INSPECTION (HFEC & US) OF STRINGER
AND STRINGER COUPLING AT FR 26, STR 5 (LH/RH).
NOTE:
ROTO TEST INSPECTION TO BE PERFORMED IN CASE US
INSPECTION IS NOT FEASIBLE ACCORDING TO NTM.
PREP.: INSULATION Z230;
LINING Z230;
OVERHEAD STOWAGE BINS Z230;
FC OPTIMIZED:
T: 39700 FC
OR
119300 FH
I: 14100 FC
FH OPTIMIZED:
T: 31700 FC
OR
215500 FH
ALI
532100-220-855
ALI REFERENCE:
532195-01-02
I: 13700 FC
FC OPTIMIZED:
T: 37700 FC
OR
113100 FH
*
15.00
*
0.04
1
1
3.73 GROUP 33B
3.73 PRE 204499
(53-3251),
(53-3252)
I: 13700 FC
ACCESS: 831
R
532199-01-2
841
253 FORWARD FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (HFEC & US) OF STRINGERS
AND STRINGER COUPLINGS AT FR 37.1, STR 1 - STR 13
(LH/RH).
FH OPTIMIZED:
T: 28000 FC
OR
190200 FH
I:
NOTE:
ROTO TEST INSPECTION TO BE PERFORMED IN CASE US
INSPECTION IS NOT FEASIBLE ACCORDING TO NTM.
PREP.: INSULATION Z250;
LINING Z250;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 831
841
STRUCTURE : FUSELAGE
ALI WFD
532100-220-849
ALI REFERENCE:
532199-01-02
8500 FC
OR
57600 FH
FC OPTIMIZED:
T: 33300 FC
OR
108700 FH
I:
9400 FC
OR
30700 FH
REV. DATE: JUL 01/21
SECTION:
3 -53
*
30.00
*
*
0.02
0.02
PAGE 61
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
R
532199-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
253 FORWARD FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (HFEC & US) OF STRINGERS
AND STRINGER COUPLINGS AT FR 37.1, STR 1 - STR 13
(LH/RH).
FH OPTIMIZED:
T: 21400 FC
OR
145400 FH
I:
NOTE:
ROTO TEST INSPECTION TO BE PERFORMED IN CASE US
INSPECTION IS NOT FEASIBLE ACCORDING TO NTM.
ACCESS: 831
841
I:
196 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON
ARCH MEMBER AT Y=-1445.
ACCESS: 196AB
533001-01-4
ALI WFD
REFERENCE
532100-220-849
4900 FC
OR
16200 FH
MRB
5500 FC
533100-220-809
AF
DET
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON
ARCH MEMBER AT Y=-1445.
T: 19900 FC
I:
MRB
5500 FC
533100-220-809
533002-01-2
149 CENTER FUSELAGE
DET
T: 20000 FC
DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT FR
47, T-SECTION FLANGE BELOW ATTACHMENT OF LONGITUDINAL
WEB AT Y=-493.
I: 16200 FC
ACCESS: 196AB
* * * * *
STRUCTURE : FUSELAGE
AF
MRB
533100-220-810
C O N T I N U E D
3.73 GROUP 33C
3.73 PRE 204499
(53-3251),
(53-3252)
OR
GROUP 33D
PRE 204499
(53-3251),
(53-3252)
*
*
0.02
0.02
1
0.25 GROUP 33A
PRE 41410
PRE 43451
(53-3049)
*
2.51
1
0.25 GROUP 33A
POST 41410
PRE 43451
(53-3049)
*
0.25
1
0.10 GROUP 33A
PRE 41410
PRE 43727
(53-3050)
OR
GROUP 33B
2.51 PRE 41410
PRE 43727
MRB REFERENCE:
533002-01-2
196BB
APPLICABILITY
30.00
MRB REFERENCE:
533001-01-4
ACCESS: 196EB
M/H
*
MRB REFERENCE:
533001-01-2
196BB
196 CENTER FUSELAGE
1
1
4400 FC
OR
30500 FH
T: 19900 FC
I:
MEN
ALI REFERENCE:
532199-01-03
FC OPTIMIZED:
T: 25400 FC
OR
83100 FH
PREP.: INSULATION Z250;
LINING Z250;
OVERHEAD STOWAGE BINS Z250;
533001-01-2
SOURCE
*
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 62
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533002-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
(53-3050)
533002-01-4
149 CENTER FUSELAGE
AF
DET
T: 20000 FC
DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT FR
47, T-SECTION FLANGE BELOW ATTACHMENT OF LONGITUDINAL
WEB AT Y=-493.
I: 16200 FC
MRB
533100-220-810
MRB REFERENCE:
533002-01-4
ACCESS: 196GB
533003-01-2
*
149 CENTER FUSELAGE
AF
DET
197
198 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE, FR
53.2 WEB AT Y=-1042, Y=-728.7 AND Y=728.7 BELOW
LONGITUDINAL WEB ATTACHMENT.
T: 20000 FC
MRB
I: 20000 FC
533100-220-811
MRB REFERENCE:
533003-01-2
ACCESS: 197AB
533004-01-2
197 CENTER FUSELAGE
AF
198
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE AFT OF FR 53.8, T-SECTION JUNCTION ON
LONGITUDINAL BEAM, LH/RH.
DET
T: 19900 FC
I:
MRB
5500 FC
533100-220-812
MRB REFERENCE:
533004-01-2
ACCESS: 197GB
198GB
533005-01-2
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
ACCESS: 191AB
192AT
197AT
198AT
* * * * *
STRUCTURE : FUSELAGE
1
191AT
192BB
197FB
198GB
191BB
192CB
197GB
198HB
T: 16400 FC
I:
ALI
4800 FC
533100-220-813
ALI REFERENCE:
533005-01-02
191CB
*
0.10 GROUP 33A
0.10 PRE 43727
0.10 (53-3050)
OR
GROUP 33B
PRE 43727
2.75 (53-3050)
1
1
0.10 GROUP 33A
0.10
*
*
1.60
1.60
1
1
1
1
0.20 A330-200F
0.20
0.20
0.20
*
*
*
*
197HB
C O N T I N U E D
1
1
1
0.10 GROUP 33A
POST 41410
PRE 43727
(53-3050)
OR
GROUP 33B
1.50 POST 41410
PRE 43727
(53-3050)
10.30
7.05
7.40
5.80
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 63
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533005-01-2
533005-01-3
ZONE
* * * * *
533005-01-5
191AT
192BB
197FB
198GB
191BB
192CB
197GB
198HB
191AT
192BB
197FB
198GB
191BB
192CB
197GB
198HB
REFERENCE
T: 41300 FC
MRB
I: 41300 FC
533100-220-813
MRB REFERENCE:
533005-01-3
191CB
197HB
T: 21900 FC
MRB
I: 21900 FC
533100-220-813
MRB REFERENCE:
533005-01-4
191CB
197HB
T: 14400 FC
MRB
I: 14400 FC
533100-220-813
MRB REFERENCE:
533005-01-5
191CB
MEN
197HB
C O N T I N U E D
1
1
1
1
M/H
APPLICABILITY
T: 14400 FC
I:
ALI
MRB
533100-220-813
4800 FC
ALI REFERENCE:
533005-01-02
REV. DATE: JUL 01/21
SECTION:
0.20 GROUP 33A
0.20
0.20
0.20
*
*
*
*
10.30
7.05
7.40
5.80
1
1
1
1
0.20
0.20
0.20
0.20
*
*
*
*
10.30
7.05
7.40
5.80
1
1
1
1
*
*
*
*
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
* * * * *
STRUCTURE : FUSELAGE
191BB
192CB
197GB
198HB
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
ACCESS: 191AB
192AT
197AT
198AT
533005-01-6
191AT
192BB
197FB
198GB
SOURCE
* * * * *
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
ACCESS: 191AB
192AT
197AT
198AT
R
C O N T I N U E
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
ACCESS: 191AB
192AT
197AT
198AT
533005-01-4
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
1
1
1
1
GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
0.20 GROUP 32A
0.20 OR
0.20 A330-900
0.20
10.30
7.05
7.40
5.80
0.20 GROUP 32E
0.20
0.20
0.20
* * * * *
3-53
PAGE 64
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533005-01-6
ZONE
* * * * *
ACCESS: 191AB
192AT
197AT
198AT
533005-01-7
533005-01-8
191BB
192CB
197GB
198HB
191AT
192BB
197FB
198GB
191BB
192CB
197GB
198HB
191AT
192BB
197FB
198GB
191BB
192CB
197GB
198HB
REFERENCE
MRB REFERENCE:
533005-01-5
191CB
197HB
T: 16400 FC
I:
4800 FC
ALI
MRB
533100-220-813
ALI REFERENCE:
533005-01-02
MRB REFERENCE:
533005-01-4
191CB
197HB
T: 10100 FC
MRB
I: 10100 FC
533100-220-813
MRB REFERENCE:
533005-01-6
191CB
MEN
M/H
*
*
*
*
10.30
7.05
7.40
5.80
1
1
1
1
*
*
*
*
1
1
1
1
*
*
*
*
197HB
147 CENTER FUSELAGE
AF
148
149 DETAILED INSPECTION OF BELLY FAIRING SUPPORT
197 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB.
198
ACCESS: 147BB
148BB
197AB
197HB
198AT
STRUCTURE : FUSELAGE
191AT
192BB
197FB
198GB
SOURCE
APPLICABILITY
* * * * *
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO FR 38 AND FROM
FR 53.6 TO FR 56.
ACCESS: 191AB
192AT
197AT
198AT
533006-01-1
C O N T I N U E
191 CENTER FUSELAGE
AF
DET
192
197 DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING
198 SEALING LIP ATTACHMENT FROM FR 37.1 TO 38 AND FROM FR
53.6 TO 56.
ACCESS: 191AB
192AT
197AT
198AT
N
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
147BT
148BT
197AT
734
744
197BB
197EB
197FB
198BB
198EB
198GB
198HB
DET
T:
3 YE
I:
3 YE
MRB
533100-220-805
MRB REFERENCE:
533006-01-1
197GB
REV. DATE: JUL 01/21
SECTION:
3 -53
1
1
1
1
1
0.20 GROUP 33E
0.20
0.20
0.20
10.30
7.05
7.40
5.80
0.20 A330-800
0.20
0.20
0.20
10.30
7.05
7.40
5.80
0.15 PRE 50675
0.15 (53-3166)
0.15
0.15
0.15
*
*
*
2.75
2.75
13.90
*
9.55
PAGE 65
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533006-01-2
ZONE
147 CENTER FUSELAGE
AF
148
149 DETAILED INSPECTION OF BELLY FAIRING SUPPORT
197 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB.
198
ACCESS: 147BB
148BB
197AB
197HB
198AT
533007-01-1
147BT
148BT
197AT
734
744
197BB
197EB
197FB
198BB
198EB
198GB
198HB
191AT
192BB
191BB
192CB
191CB
DET
T:
6 YE
I:
6 YE
SOURCE
MRB
REFERENCE
533100-220-805
MRB REFERENCE:
533006-01-2
MEN
M/H
1
1
1
1
1
0.15
0.15
0.15
0.15
0.15
*
*
*
197GB
191 CENTER FUSELAGE
AF
192
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE, FR 37.4 WEB.
ACCESS: 191AB
192AT
STRUCTURE : FUSELAGE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
*
DET
T:
3 YE
I:
3 YE
MRB
533100-220-806
1
1
MRB REFERENCE:
533007-01-1
191DB
*
*
REV. DATE: JUL 01/21
SECTION:
3 -53
APPLICABILITY
A330-200
POST 50675
(53-3166)
OR
A330-300
POST 50675
2.75 (53-3166)
2.75
13.90
9.55
0.10 GROUP 32A
0.10 PRE 43352
(53-3038)
PRE 50675
(53-3166)
12.55 OR
7.05 GROUP 32E
PRE 43352
(53-3038)
PRE 50675
(53-3166)
OR
GROUP 33C
PRE 43352
(53-3038)
PRE 50675
(53-3166)
OR
GROUP 33D
PRE 43352
(53-3038)
PRE 50675
(53-3166)
OR
GROUP 33E
PRE 43352
(53-3038)
PRE 50675
(53-3166)
PAGE 66
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533007-01-2
ZONE
191 CENTER FUSELAGE
AF
192
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE, FR 37.4 WEB.
ACCESS: 191AB
192AT
533007-01-3
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
191AT
192BB
191BB
192CB
191CB
DET
T:
6 YE
I:
6 YE
STRUCTURE : FUSELAGE
191BB
192CB
191CB
533100-220-806
191DB
MEN
1
1
MRB REFERENCE:
533007-01-2
*
*
DET
T:
I:
191AT
192BB
MRB
REFERENCE
191DB
191 CENTER FUSELAGE
AF
192
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE, FR 37.4 WEB.
ACCESS: 191AB
192AT
SOURCE
6 YE
OR
17100 FC
MRB
6 YE
OR
3800 FC
REV. DATE: JUL 01/21
533100-220-806
1
1
MRB REFERENCE:
533007-01-2
533007-01-3
*
*
SECTION:
3 -53
M/H
APPLICABILITY
0.10 GROUP 32A
0.10 PRE 43352
(53-3038)
POST 50675
(53-3166)
12.55 OR
7.05 GROUP 32E
PRE 43352
(53-3038)
POST 50675
(53-3166)
OR
GROUP 33C
PRE 43352
(53-3038)
POST 50675
(53-3166)
OR
GROUP 33D
PRE 43352
(53-3038)
POST 50675
(53-3166)
OR
GROUP 33E
PRE 43352
(53-3038)
POST 50675
(53-3166)
0.10 GROUP 33A
0.10 PRE 43352
(53-3038)
POST 50675
(53-3166)
12.55 OR
7.05 GROUP 33B
PRE 43352
(53-3038)
POST 50675
(53-3166)
PAGE 67
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533007-01-4
ZONE
191 CENTER FUSELAGE
AF
192
DETAILED INSPECTION OF BELLY FAIRING SUPPORT
STRUCTURE, FR 37.4 WEB.
ACCESS: 191AB
192AT
533008-01-1
533009-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
191AT
192BB
191BB
192CB
191CB
DET
T:
I:
191DB
190 CENTER FUSELAGE
AF
3 YE
OR
17100 FC
T:
3 YE
DETAILED INSPECTION OF BELLY FAIRING PANELS AND
FASTENERS AT WING UPPER SURFACE TO FUSELAGE JUNCTION,
FROM WING LEADING EDGE TO TRAILING EDGE, LH/RH.
I:
3 YE
FH OPTIMIZED:
T: 15800 FC
OR
95000 FH
I:
PREP.: BOLTS;
INSULATION Z250;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251JC
252JC
MRB
REFERENCE
533100-220-806
1
1
*
*
MRB
533100-220-808
M/H
APPLICABILITY
0.10 GROUP 33A
0.10 PRE 43352
(53-3038)
PRE 50675
(53-3166)
12.55 OR
7.05 GROUP 33B
PRE 43352
(53-3038)
PRE 50675
(53-3166)
1
1.50 ALL
1
1
1
1
4.00
4.00
4.00
4.00
MRB REFERENCE:
533008-01-1
ALI WFD
533100-250-812
ALI REFERENCE:
533009-01-01
9100 FC
OR
54800 FH
*
FC OPTIMIZED:
T: 18400 FC
OR
55300 FH
251VW
252VW
MEN
MRB REFERENCE:
533007-01-1
533007-01-3
3 YE
OR
3800 FC
DET
251 CENTER FUSELAGE
NDT SDI
252
253 SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
254 CIRCUMFERENTIAL BUTT JOINT AT FR 45, BETWEEN STR 3
AND 5, AND BETWEEN STR 11 AND 13, LH/RH.
SOURCE
GROUP 33A
PRE 52911
(53-3144)
OR
GROUP 33B
PRE 52911
30.00 (53-3144)
*
*
0.14
0.14
1
1
1
1
4.00
4.00
4.00
4.00
I: 10100 FC
OR
30300 FH
533009-01-2
251 CENTER FUSELAGE
NDT SDI
252
253 SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
254 CIRCUMFERENTIAL BUTT JOINT AT FR 45, BETWEEN STR 3
AND 5, AND BETWEEN STR 11 AND 13, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 17700 FC
OR
115500 FH
ALI WFD
533100-250-812
ALI REFERENCE:
533009-01-02
GROUP 32A
PRE 49202
PRE 52911
(53-3144)
OR
GROUP 32A
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 68
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533009-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PREP.: BOLTS;
INSULATION Z250;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251JC
252JC
SOURCE
I:
251VW
252VW
9700 FC
OR
63400 FH
*
FC OPTIMIZED:
T: 21600 FC
OR
75800 FH
30.00 POST 50755
PRE 56001
(53-3169)
*
*
0.14
0.14
1
1
1
1
4.00
4.00
4.00
4.00
*
30.00
*
*
0.14
0.14
1
1
1
1
4.00
4.00
4.00
4.00
*
30.00
I: 11200 FC
OR
39300 FH
533009-01-3
251 CENTER FUSELAGE
NDT SDI
252
253 SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
254 CIRCUMFERENTIAL BUTT JOINT AT FR 45, BETWEEN STR 3
AND 5, AND BETWEEN STR 11 AND 13, LH/RH.
FH OPTIMIZED:
T: 13000 FC
OR
78100 FH
I:
PREP.: BOLTS;
INSULATION Z250;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251JC
252JC
251 CENTER FUSELAGE
NDT SDI
252
253 SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
254 CIRCUMFERENTIAL BUTT JOINT AT FR 45, BETWEEN STR 3
AND 5, AND BETWEEN STR 11 AND 13, LH/RH.
PREP.: BOLTS;
INSULATION Z250;
OVERHEAD STOWAGE BINS Z250;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
533100-250-812
ALI REFERENCE:
533009-01-03
7400 FC
OR
44800 FH
FC OPTIMIZED:
T: 15100 FC
OR
45500 FH
251VW
252VW
I:
533009-01-4
ALI WFD
8200 FC
OR
24800 FH
FH OPTIMIZED:
T: 13300 FC
OR
80100 FH
I:
GROUP 33D
PRE 49202
PRE 52911
(53-3144)
ALI WFD
533100-250-812
ALI REFERENCE:
533009-01-04
7500 FC
OR
45400 FH
GROUP 33C
PRE 49202
PRE 52911
(53-3144)
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 69
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533009-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
ACCESS: 251JC
252JC
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.14
0.14
1
2.00 GROUP 33A
OR
GROUP 33B
* * * * *
251VW
252VW
FC OPTIMIZED:
T: 15500 FC
OR
46600 FH
I:
533010-01-1
SOURCE
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 45 FROM CROWN CENTRELINE
TO STR 3, FROM STR 5 TO STR 11 AND FROM STR 13 TO STR
17, LH/RH.
PREP.: BOLTS;
8400 FC
OR
25200 FH
FH OPTIMIZED:
T: 32100 FC
OR
192600 FH
ALI WFD
533100-250-804
ALI REFERENCE:
533010-01-01
I: 16600 FC
OR
100100 FH
*
TBD
FC OPTIMIZED:
T: 37300 FC
OR
112100 FH
I: 18500 FC
OR
55500 FH
533010-01-3
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 45 FROM CROWN CENTRELINE
TO STR 3, FROM STR 5 TO STR 11 AND FROM STR 13 TO STR
17, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 27200 FC
OR
163600 FH
ALI WFD
533100-250-804
1
2.00 GROUP 33D
PRE 49202
ALI REFERENCE:
533010-01-03
I: 13600 FC
OR
81900 FH
*
TBD
FC OPTIMIZED:
T: 31700 FC
OR
95300 FH
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 70
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533010-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 15100 FC
OR
45400 FH
533010-01-4
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 45 FROM CROWN CENTRELINE
TO STR 3, FROM STR 5 TO STR 11 AND FROM STR 13 TO STR
17, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 27900 FC
OR
167600 FH
ALI WFD
533100-250-804
1
2.00 GROUP 33C
PRE 49202
ALI REFERENCE:
533010-01-04
I: 13800 FC
OR
83100 FH
*
TBD
FC OPTIMIZED:
T: 32500 FC
OR
97600 FH
I: 15300 FC
OR
46100 FH
533014-01-1
147 CENTER FUSELAGE
NDT SDI
148
SPECIAL DETAILED INSPECTION (HFEC) OF MAIN LANDING
GEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS
AFT OF FR 47 DATUM, LH/RH.
T: 33200 FC
I:
ALI
5700 FC
533100-250-807
ALI REFERENCE:
533014-01-01
ACCESS: 734
744
R
533015-02-1
*
*
147 CENTER FUSELAGE
NDT SDI
148
SPECIAL DETAILED INSPECTION (HFEC) OF MAIN LANDING
GEAR BAY, LOWER FLANGE OF GANTRY Y=1959 AT FR 48
LEVEL, LH/RH.
T: 18300 FC
I:
ALI
6100 FC
533100-250-867
STRUCTURE : FUSELAGE
1
1
ALI REFERENCE:
533015-02-01
ACCESS: 734
744
* * * * *
1
1
*
*
C O N T I N U E D
0.40 GROUP 32A
0.40 PRE 45307 S13490
OR
GROUP 33A
OR
GROUP 33B
0.15 PRE 45307 S13490
0.15
0.58 A330-200
0.58 OR
GROUP 33A
POST 42418 S11929
OR
GROUP 33B
0.15 OR
0.15 GROUP 33C
OR
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 71
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533015-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
GROUP 33D
OR
GROUP 33E
OR
A330-800
OR
A330-900
OR
A330-200F
D
533015-03-6
R
533016-01-2
************** TASK DELETED **************
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 38, FROM CROWN CENTERLINE
TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
FH OPTIMIZED:
T: 26100 FC
OR
177200 FH
I:
PREP.: BOLTS;
ALI WFD
533100-250-808
1
ALI REFERENCE:
533016-01-02
3800 FC
OR
25900 FH
*
8.80 GROUP 33D
OR
GROUP 33E
TBD
FC OPTIMIZED:
T: 33000 FC
OR
99000 FH
I:
R
533016-01-6
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 38, FROM CROWN CENTERLINE
TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
4200 FC
OR
14000 FH
FH OPTIMIZED:
T: 26700 FC
OR
181200 FH
I:
ALI WFD
533100-250-808
1
8.80 GROUP 33C
ALI REFERENCE:
533016-01-01
3900 FC
OR
26500 FH
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 72
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533016-01-6
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 33700 FC
OR
101300 FH
I:
N
533016-01-7
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 38, FROM CROWN CENTERLINE
TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
4300 FC
OR
14300 FH
FH OPTIMIZED:
T: 29400 FC
OR
199500 FH
I:
PREP.: BOLTS;
ALI WFD
533100-250-808
1
ALI REFERENCE:
533016-01-04
4100 FC
OR
28300 FH
*
8.80 GROUP 33A
OR
GROUP 33B
PRE 44687
TBD
FC OPTIMIZED:
T: 37100 FC
OR
111500 FH
I:
N
533016-01-8
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 38, FROM CROWN CENTERLINE
TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
4600 FC
OR
15200 FH
FH OPTIMIZED:
T: 37100 FC
OR
251100 FH
I:
ALI WFD
533100-250-808
1
8.80 GROUP 33B
POST 44687
ALI REFERENCE:
533016-01-05
4800 FC
OR
33000 FH
*
TBD
FC OPTIMIZED:
T: 37100 FC
OR
251100 FH
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 73
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533016-01-8
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
200 CENTER FUSELAGE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
533017-01-2
SOURCE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
PREP.: BOLTS;
4800 FC
OR
33000 FH
FH OPTIMIZED:
T: 19500 FC
OR
117300 FH
ALI WFD
533100-250-863
1
ALI REFERENCE:
533017-01-02
I: 10100 FC
OR
60900 FH
*
10.64 GROUP 33A
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 22700 FC
OR
68300 FH
I: 11200 FC
OR
33700 FH
533017-01-3
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 26200 FC
OR
157400 FH
ALI WFD
533100-250-863
1
ALI REFERENCE:
533017-01-03
I: 10100 FC
OR
60900 FH
*
10.64 GROUP 33B
PRE 44723
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 30500 FC
OR
91700 FH
I: 11200 FC
OR
33700 FH
STRUCTURE : FUSELAGE
REV. DATE: JUL 0 1/21
SECTION:
3-53
PAGE 74
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533017-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 33100 FC
OR
198900 FH
SOURCE
ALI WFD
REFERENCE
533100-250-863
MEN
1
ALI REFERENCE:
533017-01-04
I: 14300 FC
OR
85900 FH
*
M/H
APPLICABILITY
10.64 GROUP 33B
POST 44723
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 38600 FC
OR
115800 FH
I: 15800 FC
OR
47600 FH
533017-01-5
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 30400 FC
OR
182600 FH
ALI WFD
533100-250-863
1
ALI REFERENCE:
533017-01-05
I: 13400 FC
OR
80700 FH
*
10.64 GROUP 33C
PRE 49202
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 35400 FC
OR
106400 FH
I: 14900 FC
OR
44700 FH
533017-01-6
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 29700 FC
OR
178200 FH
ALI WFD
533100-250-863
ALI REFERENCE:
533017-01-06
1
10.64 GROUP 33D
PRE 49202
PRE 49403
(53-3127),
(53-3143)
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 75
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533017-01-6
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PREP.: BOLTS;
I: 13200 FC
OR
79500 FH
*
TBD
FC OPTIMIZED:
T: 34600 FC
OR
103800 FH
I: 14700 FC
OR
44100 FH
533017-01-7
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3, FROM CROWN
CENTERLINE TO STR 4, FROM STR 5 TO STR 11 AND FROM
STR 13 TO STR 17, EXTERNAL SURFACE, LH/RH.
FH OPTIMIZED:
T: 38400 FC
OR
249900 FH
ALI WFD
533100-250-863
ALI REFERENCE:
533017-01-07
I: 15900 FC
OR
103400 FH
PREP.: BOLTS;
1
*
10.64 GROUP 32A
PRE 49202
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 46800 FC
OR
164100 FH
I: 18300 FC
OR
64100 FH
533018-01-5
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 34900 FC
OR
227100 FH
ALI WFD
533100-250-810
1
ALI REFERENCE:
533018-01-01
I: 12000 FC
OR
78400 FH
*
9.87 GROUP 32A
PRE 49202
POST 40161
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 76
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533018-01-5
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 42600 FC
OR
149100 FH
I: 13800 FC
OR
48600 FH
533018-01-6
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 40800 FC
OR
245200 FH
ALI WFD
533100-250-810
1
ALI REFERENCE:
533018-01-02
I: 18300 FC
OR
110300 FH
*
9.87 GROUP 33D
PRE 49202
TBD
FC OPTIMIZED:
T: 47600 FC
OR
142800 FH
I: 20400 FC
OR
61200 FH
533018-01-7
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 41800 FC
OR
251300 FH
ALI WFD
533100-250-810
1
ALI REFERENCE:
533018-01-03
I: 18600 FC
OR
112000 FH
*
9.87 GROUP 33C
PRE 49202
PRE 40161
TBD
FC OPTIMIZED:
T: 48700 FC
OR
146300 FH
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 77
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533018-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 20700 FC
OR
62100 FH
533018-01-8
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
FH OPTIMIZED:
T: 28400 FC
OR
170900 FH
I:
PREP.: BOLTS;
ALI WFD
533100-250-810
1
9.87 GROUP 33A
PRE 40556
ALI REFERENCE:
533018-01-04
5000 FC
OR
30200 FH
*
TBD
FC OPTIMIZED:
T: 33100 FC
OR
99500 FH
I:
533018-01-9
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
5600 FC
OR
16800 FH
FH OPTIMIZED:
T: 30900 FC
OR
185800 FH
ALI WFD
533100-250-810
1
9.87 GROUP 33A
POST 40556
ALI REFERENCE:
533018-01-05
I: 17800 FC
OR
106800 FH
*
TBD
FC OPTIMIZED:
T: 36000 FC
OR
108200 FH
I: 19700 FC
OR
59200 FH
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 78
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533018-01-11
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 28300 FC
OR
169900 FH
SOURCE
ALI WFD
REFERENCE
533100-250-810
MEN
1
M/H
APPLICABILITY
9.87 GROUP 33B
POST 40161
ALI REFERENCE:
533018-01-07
I: 10300 FC
OR
62200 FH
*
TBD
FC OPTIMIZED:
T: 33000 FC
OR
99000 FH
I: 11500 FC
OR
34500 FH
533018-01-12
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54, FROM CROWN CENTERLINE
TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE,
LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 26400 FC
OR
158600 FH
I:
ALI WFD
533100-250-810
1
ALI REFERENCE:
533018-01-08
9500 FC
OR
57400 FH
*
9.87 GROUP 33C
PRE 49202
POST 40161
TBD
FC OPTIMIZED:
T: 30700 FC
OR
92300 FH
I: 10600 FC
OR
31800 FH
533021-01-3
147 CENTER FUSELAGE
NDT SDI
148
149 SPECIAL DETAILED INSPECTION (HFEC) OF RADII OF TEE
FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL
BEAMS Y=953 AND Y=450, BELOW PRESSURE FLOOR, AT
PRESSURE BULKHEAD FR.53.2, LH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 7800 FC
OR
51400 FH
ALI
533100-250-856
ALI REFERENCE:
533021-01-03
1
1
1
0.10 GROUP 32E
0.10 OR
0.10 GROUP 33E
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 79
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533021-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
I:
ACCESS: 734
744
FC OPTIMIZED:
T: 8650 FC
OR
28300 FH
I:
147 CENTER FUSELAGE
NDT SDI
148
149 SPECIAL DETAILED INSPECTION (BORESCOPE) OF RADII OF
TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL
BEAMS Y=953 AND Y=450, BELOW PRESSURE FLOOR, AT
PRESSURE BULKHEAD FR.53.2, LH.
*
1.00
*
*
0.15
0.15
1
1
1
0.10 GROUP 32E
0.10 OR
0.10 GROUP 33E
ACCESS: 734
744
*
*
0.15
0.15
I:
ALI
533100-290-809
ALI REFERENCE:
533021-02-03
5200 FC
OR
34300 FH
FC OPTIMIZED:
T: 8650 FC
OR
28300 FH
I:
200 CENTER FUSELAGE
NDT SDI
253
254 SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 5 FROM FR 38 TO 45,
INTERNAL AND EXTERNAL, LH/RH.
5750 FC
OR
18900 FH
FH OPTIMIZED:
T: 7800 FC
OR
51400 FH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533021-01-3.
5750 FC
OR
18900 FH
T: 33800 FC
ALI
I: 10200 FC
533100-270-826
ALI REFERENCE:
533022-01-01
PREP.: GALLEYS AND TOILETS (IF INSTALLED);
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
STRUCTURE : FUSELAGE
APPLICABILITY
5200 FC
OR
34300 FH
PREP.: GREEN RESERVOIR;
533022-01-1
M/H
* * * * *
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533021-02-3.
533021-02-3
MEN
1
1
1
*
REV. DATE: JUL 01/21
SECTION:
3 -53
16.13 GROUP 32A
16.13 OR
16.13 GROUP 33A
OR
GROUP 33B
OR
TBD GROUP 33C
OR
GROUP 33D
PAGE 80
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533023-02-1
533023-02-2
533024-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 5 FROM FR 45 TO 53.3,
LH/RH.
T: 24000 FC
OR
73200 FH
253 CENTER FUSELAGE
NDT
254
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 5 FROM FR 45 TO FR
53.3, LH/RH.
T: 33800 FC
200 CENTER FUSELAGE
NDT
SDI
I:
SOURCE
ALI
6300 FC
OR
19100 FH
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13, FROM FR 38 TO 45,
LH/RH.
FH OPTIMIZED:
T: 30000 FC
OR
192300 FH
I:
533100-270-858
MEN
M/H
APPLICABILITY
1
1
12.10 A330-200F
12.10
1
1
12.10 GROUP
12.10 OR
GROUP
OR
GROUP
OR
GROUP
OR
GROUP
ALI REFERENCE:
533023-01-02
ALI
I: 10200 FC
SDI
REFERENCE
533100-270-858
ALI REFERENCE:
533023-02-01
ALI WFD
533100-270-827
32A
33A
33B
33C
33D
1
2.86 GROUP 32A
OR
GROUP 33A
OR
GROUP 33B
1
2.86 GROUP 33C
OR
GROUP 33D
OR
GROUP 33E
ALI REFERENCE:
533024-01-01
8500 FC
OR
55200 FH
FC OPTIMIZED:
T: 36600 FC
OR
112000 FH
I:
533024-01-2
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13, FROM FR 38 TO 45,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
9700 FC
OR
31300 FH
FH OPTIMIZED:
T: 27500 FC
OR
165300 FH
ALI WFD
533100-270-827
ALI REFERENCE:
533024-01-02
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 81
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533024-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
8100 FC
OR
48800 FH
FC OPTIMIZED:
T: 32100 FC
OR
96300 FH
I:
533024-01-5
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13, FROM FR 38 TO 45,
LH/RH.
533025-01-2
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13 FROM FR 45 TO FR
53.3, LH/RH.
9000 FC
OR
27000 FH
T: 32100 FC
OR
192600 FH
I:
ALI WFD
533100-270-827
1
2.86 A330-900
ALI REFERENCE:
533024-01-05
9200 FC
OR
62900 FH
FH OPTIMIZED:
T: 31500 FC
OR
189300 FH
ALI
533100-270-828
ALI REFERENCE:
533025-01-02
I: 11500 FC
OR
69200 FH
1
1
24.20 GROUP 33C
24.20 PRE 48829
OR
GROUP 33D
PRE 48829
FC OPTIMIZED:
T: 36700 FC
OR
110300 FH
I: 12800 FC
OR
38400 FH
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 82
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533025-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13 FROM FR 45 TO FR
53.3, LH/RH.
FH OPTIMIZED:
T: 36200 FC
OR
180000 FH
SOURCE
ALI
REFERENCE
533100-270-828
MEN
M/H
APPLICABILITY
1
1
24.20 GROUP 33C
24.20 POST 48829
OR
GROUP 33D
POST 48829
1
1
24.20 GROUP 33B
24.20
ALI REFERENCE:
533025-01-01
I: 13100 FC
OR
79000 FH
FC OPTIMIZED:
T: 42100 FC
OR
126500 FH
I: 14600 FC
OR
43800 FH
533025-01-5
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 13 FROM FR 45 TO FR
53.3, LH/RH.
FH OPTIMIZED:
T: 36200 FC
OR
180000 FH
ALI
533100-270-828
ALI REFERENCE:
533025-01-01
I: 13100 FC
OR
79000 FH
FC OPTIMIZED:
T: 42100 FC
OR
126500 FH
I: 14600 FC
OR
43800 FH
533026-01-1
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 36500 FC
OR
219100 FH
ALI WFD
533100-270-831
ALI REFERENCE:
533026-01-01
1
1
1.43 GROUP 33A
1.43 PRE 40370
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 83
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533026-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
9100 FC
OR
55100 FH
FC OPTIMIZED:
T: 42500 FC
OR
127600 FH
I: 10200 FC
OR
30600 FH
533026-01-2
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
FH OPTIMIZED:
T: 30900 FC
OR
185800 FH
I:
ALI WFD
533100-270-831
1
1
1.43 GROUP 33A
1.43 POST 40370
OR
GROUP 33B
1
1
1.43 GROUP 33C
1.43 OR
GROUP 33D
OR
GROUP 33E
ALI REFERENCE:
533026-01-02
9000 FC
OR
54200 FH
FC OPTIMIZED:
T: 36000 FC
OR
108200 FH
I: 10000 FC
OR
30000 FH
533026-01-3
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 25100 FC
OR
151000 FH
I:
ALI WFD
533100-270-831
ALI REFERENCE:
533026-01-03
7100 FC
OR
42800 FH
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 84
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533026-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 29300 FC
OR
88000 FH
I:
533026-01-4
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
7900 FC
OR
23700 FH
FH OPTIMIZED:
T: 27300 FC
OR
177500 FH
I:
ALI WFD
533100-270-831
ALI REFERENCE:
533026-01-04
1
1
1.43 GROUP 32A
1.43
1
1
1.43 A330-200F
1.43
7400 FC
OR
48400 FH
FC OPTIMIZED:
T: 33300 FC
OR
116500 FH
I:
533026-01-6
533026-01-7
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
T: 27700 FC
OR
83300 FH
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 38 TO 45,
LH/RH.
FH OPTIMIZED:
T: 27400 FC
OR
164800 FH
* * * * *
STRUCTURE : FUSELAGE
8500 FC
OR
30000 FH
C O N T I N U E D
I:
ALI WFD
533100-270-831
ALI REFERENCE:
533026-01-06
7900 FC
OR
24100 FH
ALI WFD
533100-270-831
1
1
13.20 A330-900
13.20
ALI REFERENCE:
533026-01-07
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 85
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533026-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
8100 FC
OR
55200 FH
FC OPTIMIZED:
T: 28900 FC
OR
86900 FH
I:
533027-01-1
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 45 TO 53.3,
LH/RH.
8500 FC
OR
25700 FH
FH OPTIMIZED:
T: 35700 FC
OR
214400 FH
ALI WFD
533100-270-832
1
23.33 GROUP 33A
OR
GROUP 33B
1
23.33 GROUP 33C
OR
GROUP 33D
OR
GROUP 33E
ALI REFERENCE:
533027-01-01
I: 10000 FC
OR
60100 FH
FC OPTIMIZED:
T: 41600 FC
OR
124900 FH
I: 11100 FC
OR
33300 FH
533027-01-2
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 45 TO 53.3,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 37800 FC
OR
226800 FH
ALI WFD
533100-270-832
ALI REFERENCE:
533027-01-02
I: 11500 FC
OR
69100 FH
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 86
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533027-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 44000 FC
OR
132100 FH
I: 12700 FC
OR
38300 FH
533027-01-4
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 22, FROM FR 45 TO 53.3,
LH/RH.
533028-01-1
147 CENTER FUSELAGE
NDT SDI
148
149 SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL BUTT JOINT AT STR 39 BETWEEN FR 53.2 AND
FR 53.3, LH/RH.
NOTE:
FOR AIRCRAFT POST 42607 THRESHOLD IS TO BE COUNTED
FROM SB 53-3021 EMBODIMENT.
ACCESS: 734
744
T: 17200 FC
OR
51700 FH
I:
ALI
533100-270-832
1
23.33 A330-200F
ALI REFERENCE:
533027-01-04
2700 FC
OR
8300 FH
FH OPTIMIZED:
T: 31300 FC
OR
180000 FH
ALI
533100-270-830
ALI REFERENCE:
533028-01-01
1
1
1
0.48 GROUP 33A
0.48 POST 42607
0.48 (53-3021)
OR
GROUP 33B
*
0.30
1
1
1
0.48 GROUP 33C
0.48 OR
0.48 GROUP 33D
I: 14600 FC
OR
99400 FH
FC OPTIMIZED:
T: 32500 FC
OR
106400 FH
I: 15300 FC
OR
50000 FH
533028-01-2
147 CENTER FUSELAGE
NDT SDI
148
149 SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL BUTT JOINT AT STR 39 BETWEEN FR 53.2 AND
FR 53.3, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 41100 FC
OR
180000 FH
ALI
533100-270-830
ALI REFERENCE:
533028-01-02
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 87
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533028-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
ACCESS: 734
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.30
1
1
0.70 GROUP 33B
0.70
*
*
3.50
3.50
1
1
0.70 A330-200
0.70 OR
GROUP 33C
OR
GROUP 33D
OR
3.50 GROUP 33E
3.50 OR
A330-800
OR
A330-900
* * * * *
I: 19400 FC
OR
131300 FH
744
FC OPTIMIZED:
T: 42700 FC
OR
139700 FH
I: 20200 FC
OR
66100 FH
533029-01-1
197 CENTER FUSELAGE
NDT SDI
198
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 44 FROM FR 53.3 TO FR
54, LH/RH.
ACCESS: 197EB
198EB
R
533029-01-2
533029-01-3
STRUCTURE : FUSELAGE
I: 10500 FC
533100-270-837
ALI REFERENCE:
533029-01-01
T: 30600 FC
ALI WFD
I: 10500 FC
533100-270-837
ALI REFERENCE:
533029-01-02
197HB
198HB
*
*
197 CENTER FUSELAGE
NDT SDI
198
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 44 FROM FR 53.3 TO FR
54, LH/RH.
* * * * *
ALI WFD
197HB
198HB
197 CENTER FUSELAGE
NDT SDI
198
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL LAP JOINT AT STR 44 FROM FR 53.3 TO FR
54, LH/RH.
ACCESS: 197EB
198EB
T: 36100 FC
C O N T I N U E D
T: 28900 FC
I:
ALI WFD
533100-270-837
8000 FC
ALI REFERENCE:
533029-01-03
REV. DATE: JUL 01/21
SECTION:
1
1
0.70 GROUP 32F
0.70
* * * * *
3 -53
PAGE 88
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533029-01-3
ZONE
* * * * *
ACCESS: 197EB
198EB
533030-01-1
533031-01-1
C O N T I N U E
T: 28900 FC
I:
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
533100-270-839
MEN
M/H
*
*
3.50
3.50
1
1
0.70 A330-200
0.70 OR
A330-300
*
*
1.90
1.90
1
1
2.68 GROUP 33A
2.68 PRE 42831
ALI REFERENCE:
533030-01-01
I:
ALI WFD
533100-250-861
APPLICABILITY
ALI REFERENCE:
533031-01-01
3300 FC
OR
22800 FH
FC OPTIMIZED:
T: 34700 FC
OR
104200 FH
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
STRUCTURE : FUSELAGE
5100 FC
FH OPTIMIZED:
T: 27500 FC
OR
186500 FH
I:
* * * * *
ALI WFD
191BT
192BT
ACCESS: 251CC
252CC
533031-01-2
REFERENCE
197HB
198HB
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
R
SOURCE
* * * * *
191 CENTER FUSELAGE
NDT SDI
192
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE
LONGITUDINAL BUTT JOINTS AT STR 30, FROM FR 38 TO FR
40.
ACCESS: 191AT
192AT
R
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E D
TBD
*
*
0.07
0.07
1
1
2.68 GROUP 33A
2.68 POST 42831
3700 FC
OR
12300 FH
FH OPTIMIZED:
T: 23400 FC
OR
158300 FH
I:
*
ALI WFD
533100-250-861
ALI REFERENCE:
533031-01-02
3400 FC
OR
23500 FH
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 89
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533031-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
FC OPTIMIZED:
T: 29500 FC
OR
88500 FH
I:
533031-01-3
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251CC
252CC
533031-01-4
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251CC
252CC
* * * * *
STRUCTURE : FUSELAGE
MEN
M/H
APPLICABILITY
*
*
0.07
0.07
1
1
2.68 GROUP 33B
2.68 PRE 44687
C O N T I N U E D
3800 FC
OR
12700 FH
FH OPTIMIZED:
T: 23800 FC
OR
161600 FH
I:
ALI WFD
533100-250-861
ALI REFERENCE:
533031-01-03
3700 FC
OR
25100 FH
FC OPTIMIZED:
T: 30100 FC
OR
90300 FH
I:
R
REFERENCE
* * * * *
ACCESS: 251CC
252CC
R
SOURCE
TBD
*
*
0.07
0.07
1
1
2.68 GROUP 33B
2.68 POST 44687
4100 FC
OR
13500 FH
FH OPTIMIZED:
T: 28000 FC
OR
189800 FH
I:
*
ALI WFD
533100-250-861
ALI REFERENCE:
533031-01-04
3900 FC
OR
26900 FH
FC OPTIMIZED:
T: 35300 FC
OR
106000 FH
*
TBD
*
*
0.07
0.07
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 90
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533031-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
533031-01-5
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
I:
ACCESS: 251CC
252CC
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
I:
1
1
ALI REFERENCE:
533031-01-05
M/H
APPLICABILITY
2.68 GROUP 33C
2.68 OR
GROUP 33D
*
TBD
*
*
0.07
0.07
1
1
2.68 GROUP 32A
2.68 PRE 48829
3600 FC
OR
12000 FH
ALI WFD
533100-250-861
ALI REFERENCE:
533031-01-06
1700 FC
OR
11700 FH
FC OPTIMIZED:
T: 36900 FC
OR
250100 FH
I:
STRUCTURE : FUSELAGE
533100-250-861
3300 FC
OR
22300 FH
FH OPTIMIZED:
T: 36900 FC
OR
250100 FH
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
ACCESS: 251CC
252CC
ALI WFD
FC OPTIMIZED:
T: 26200 FC
OR
78600 FH
I:
533031-01-6
MEN
4400 FC
OR
14500 FH
FH OPTIMIZED:
T: 20700 FC
OR
140700 FH
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
N
REFERENCE
* * * * *
I:
R
SOURCE
*
TBD
*
*
0.07
0.07
1700 FC
OR
11700 FH
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 91
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
533031-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
FH OPTIMIZED:
T: 27500 FC
OR
186600 FH
I:
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
I:
533031-01-8
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
I:
I:
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL BUTT JOINT AT FR 38, BETWEEN STR 3
AND 5,LH/RH.
STRUCTURE : FUSELAGE
1
1
APPLICABILITY
2.68 GROUP 32E
2.68 POST 50166
*
TBD
*
*
0.07
0.07
ALI WFD
533100-250-861
1
1
2.68 GROUP 32E
2.68 PRE 50166
ALI REFERENCE:
533031-01-08
3000 FC
OR
20800 FH
*
TBD
*
*
0.07
0.07
1
1
2.68 GROUP 33E
2.68
3400 FC
OR
12000 FH
FH OPTIMIZED:
T: 19200 FC
OR
130200 FH
ALI WFD
533100-250-861
ALI REFERENCE:
533031-01-09
*
C O N T I N U E D
M/H
1200 FC
OR
8200 FH
PREP.: BOLTS;
* * * * *
MEN
ALI REFERENCE:
533031-01-07
FC OPTIMIZED:
T: 28300 FC
OR
99000 FH
ACCESS: 251CC
252CC
533031-01-9
533100-250-861
1200 FC
OR
8200 FH
FH OPTIMIZED:
T: 22900 FC
OR
155000 FH
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
R
ALI WFD
REFERENCE
FC OPTIMIZED:
T: 27500 FC
OR
186600 FH
ACCESS: 251CC
252CC
R
SOURCE
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 92
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533031-01-9
* * * * *
C O N T I N U E
I:
ACCESS: 251CC
252CC
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF STRINGER
SPLICING FLANGE AREA AT CIRCUMFERENTIAL JUNCTION AT
FR 38, FROM STR 11 LH TO 11 RH.
PREP.: BOLTS;
GALLEYS AND TOILETS;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
OVERHEAD STOWAGE BINS Z250;
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY
FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1
AND FR 47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY
FAIRING, EXTERNAL SURFACE, LH/RH.
APPLICABILITY
*
*
0.07
0.07
ALI WFD
533100-250-859
1
1
2.68 GROUP 33E
2.68
ALI REFERENCE:
533032-01-03
I: 11300 FC
OR
76700 FH
T:
2.5 YE
I:
2.5 YE
MRB CPCP
533100-200-860
MRB REFERENCE:
533035-01-1
*
TBD
*
*
0.02
0.02
1
1.75 A330-200
PRE 50675
(53-3166)
OR
A330-300
PRE 50675
(53-3166)
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
* * * * *
STRUCTURE : FUSELAGE
FH OPTIMIZED:
T: 25200 FC
OR
170500 FH
I: 12600 FC
OR
41400 FH
190 CENTER FUSELAGE
TPS
M/H
3600 FC
OR
12000 FH
FC OPTIMIZED:
T: 31700 FC
OR
95300 FH
ACCESS: 832
834
533035-01-1
MEN
3300 FC
OR
22300 FH
FC OPTIMIZED:
T: 24200 FC
OR
72800 FH
I:
533032-01-7
REFERENCE
* * * * *
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z250;
N
SOURCE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 93
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
533035-01-1
* * * * *
C O N T I N U E
PREP.: FAIRING
FAIRING
FAIRING
FAIRING
533035-01-2
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
PANELS
PANELS
PANELS
PANELS
Z191;
Z192;
Z193;
Z195;
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY
FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1
AND FR 47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY
FAIRING, EXTERNAL SURFACE, LH/RH.
PANELS
PANELS
PANELS
PANELS
T:
6 YE
I:
6 YE
MRB CPCP
533100-200-860
AF
GVI
T:
5 YE
I:
5 YE
MRB CPCP
533100-200-862
56.50
1
1.75 A330-200
POST 50675
(53-3166)
OR
A330-200F
OR
A330-300
POST 50675
(53-3166)
OR
56.50 A330-800
OR
A330-900
1
MRB REFERENCE:
533036-01-1
APPLICABILITY
1.75 A330-200
PRE 50675
(53-3166)
OR
A330-300
PRE 50675
(53-3166)
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FAIRING PANELS Z197;
FAIRING PANELS Z198;
*
190 CENTER FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY
FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 47
AND FR 56 FROM Y=-2390 TO Y=2390, COVERED BY BELLY
FAIRING, EXTERNAL SURFACE, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
*
*
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY
FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 47
AND FR 56 FROM Y=-2390 TO Y=2390, COVERED BY BELLY
FAIRING, EXTERNAL SURFACE, LH/RH.
533036-01-2
M/H
MRB REFERENCE:
533035-01-2
Z191;
Z192;
Z193;
Z195;
190 CENTER FUSELAGE
TPS
MEN
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FAIRING
FAIRING
FAIRING
FAIRING
533036-01-1
REFERENCE
* * * * *
190 CENTER FUSELAGE
TPS
SOURCE
C O N T I N U E D
T:
6 YE
I:
6 YE
MRB CPCP
533100-200-862
MRB REFERENCE:
533036-01-2
1
23.50
1.75 A330-200
POST 50675
(53-3166)
OR
A330-200F
OR
A330-300
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 94
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533036-01-2
* * * * *
TPS
C O N T I N U E
SOURCE
REFERENCE
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
GVI
T:
12 YE
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY
FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR 37.1
AND FR 56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE,
EXCLUDING AREA FROM Y=-2390 TO Y=2390, LH/RH.
I:
12 YE
APPLICABILITY
AF
MRB CPCP
533100-210-817
1
POST 50675
(53-3166)
OR
23.50 A330-800
OR
A330-900
0.50 ALL
MRB REFERENCE:
533037-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
533039-01-1
*
190 CENTER FUSELAGE
TPS
M/H
* * * * *
PREP.: FAIRING PANELS Z197;
FAIRING PANELS Z198;
533037-01-1
MEN
PANELS
PANELS
PANELS
PANELS
PANELS
PANELS
Z147;
Z148;
Z191;
Z192;
Z197;
Z198;
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FRAME 53.3 FROM STRINGER 4
TO 5 AND FROM STRINGER 11 TO 13, LH/RH.
FH OPTIMIZED:
T: 16700 FC
OR
100300 FH
I:
PREP.: BOLTS;
ALI WFD
533100-250-858
ALI REFERENCE:
533039-01-01
9200 FC
OR
55400 FH
*
78.10
1
1
10.00 GROUP 33A
10.00 PRE 49403
(53-3127),
(53-3143)
*
TBD
FC OPTIMIZED:
T: 19400 FC
OR
58400 FH
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 95
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533039-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 10200 FC
OR
30700 FH
533039-01-2
253 CENTER FUSELAGE
NDT SDI
254
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FRAME 53.3 FROM STRINGER 4
TO 5 AND FROM STRINGER 11 TO 13, LH/RH.
PREP.: BOLTS;
FH OPTIMIZED:
T: 39500 FC
OR
237500 FH
ALI WFD
533100-250-858
1
1
ALI REFERENCE:
533039-01-02
I: 26400 FC
OR
158800 FH
*
10.00 GROUP 33B
10.00 PRE 44723
PRE 49403
(53-3127),
(53-3143)
TBD
FC OPTIMIZED:
T: 46100 FC
OR
138300 FH
I: 29300 FC
OR
88000 FH
533041-01-1
263 CENTER FUSELAGE
NDT SDI
264
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54 FROM STR 4 TO STR 5,
AND FROM STR 11 TO STR 13, LH/RH.
FH OPTIMIZED:
T: 13600 FC
OR
81600 FH
I:
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z260;
ACCESS: 261CC
262CC
533100-250-857
1
1
ALI REFERENCE:
533041-01-01
7100 FC
OR
43000 FH
FC OPTIMIZED:
T: 15800 FC
OR
47500 FH
I:
STRUCTURE : FUSELAGE
ALI WFD
1.67 GROUP 33A
1.67 PRE 40556
PRE 52911
(53-3144)
*
TBD
*
*
0.04
0.04
7900 FC
OR
23800 FH
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 96
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533041-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
263 CENTER FUSELAGE
NDT SDI
264
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54 FROM STR 4 TO STR 5,
AND FROM STR 11 TO STR 13, LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z260;
ACCESS: 261CC
262CC
FH OPTIMIZED:
T: 32400 FC
OR
194600 FH
SOURCE
ALI WFD
REFERENCE
533100-250-857
MEN
1
1
M/H
APPLICABILITY
1.67 GROUP 33B
1.67
ALI REFERENCE:
533041-01-02
I: 12600 FC
OR
75600 FH
*
TBD
FC OPTIMIZED:
T: 37700 FC
OR
113300 FH
*
*
0.04
0.04
1
1
1.67 GROUP 33C
1.67 PRE 49202
OR
GROUP 33D
PRE 49202
I: 13900 FC
OR
41900 FH
533041-01-3
263 CENTER FUSELAGE
NDT SDI
264
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54 FROM STR 4 TO STR 5,
AND FROM STR 11 TO STR 13, LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z260;
ACCESS: 261CC
262CC
FH OPTIMIZED:
T: 29400 FC
OR
176700 FH
ALI WFD
533100-250-857
ALI REFERENCE:
533041-01-03
I: 11400 FC
OR
68600 FH
*
TBD
FC OPTIMIZED:
T: 34300 FC
OR
102900 FH
*
*
0.04
0.04
1
1
1.67 GROUP 32A
1.67 PRE 49202
I: 12600 FC
OR
38000 FH
533041-01-4
263 CENTER FUSELAGE
NDT SDI
264
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54 FROM STR 4 TO STR 5,
AND FROM STR 11 TO STR 13, LH/RH.
FH OPTIMIZED:
T: 39100 FC
OR
254500 FH
ALI WFD
533100-250-857
ALI REFERENCE:
533041-01-04
PREP.: BOLTS;
* * * * *
STRUCTURE : FUSELAGE
*
C O N T I N U E D
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 97
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533041-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.04
0.04
1
1
1.67 GROUP 33A
1.67 POST 40556
PRE 52911
(53-3144)
* * * * *
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z260;
ACCESS: 261CC
262CC
I: 14400 FC
OR
94000 FH
FC OPTIMIZED:
T: 47700 FC
OR
167100 FH
I: 16600 FC
OR
58300 FH
533041-01-6
263 CENTER FUSELAGE
NDT SDI
264
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 54 FROM STR 4 TO STR 5,
AND FROM STR 11 TO STR 13, LH/RH.
FH OPTIMIZED:
T: 13800 FC
OR
83300 FH
I:
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
OVERHEAD STOWAGE BINS Z260;
I:
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
SPLICING INTO FR 40 FORWARD FITTING AND REAR FITTING
AT STR 21, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
* * * * *
STRUCTURE : FUSELAGE
533100-250-857
ALI REFERENCE:
533041-01-06
2300 FC
OR
13900 FH
FC OPTIMIZED:
T: 16100 FC
OR
48500 FH
ACCESS: 261CC
262CC
533042-01-1
ALI WFD
C O N T I N U E D
TBD
*
*
0.04
0.04
1
1
0.25 GROUP 33A
0.25 OR
GROUP 33B
2500 FC
OR
7700 FH
FH OPTIMIZED:
T: 35700 FC
OR
242100 FH
I:
*
ALI
533100-270-829
ALI REFERENCE:
533042-01-01
7700 FC
OR
52600 FH
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 98
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533042-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 39700 FC
OR
129900 FH
I:
533042-01-2
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
SPLICING INTO FR 40 FORWARD FITTING AND REAR FITTING
AT STR 21, LH/RH.
8600 FC
OR
28200 FH
FH OPTIMIZED:
T: 29200 FC
OR
193500 FH
I:
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
ALI
533100-270-829
ALI REFERENCE:
533042-01-02
6500 FC
OR
42500 FH
1
1
*
0.25 GROUP 32A
0.25 OR
GROUP 33C
OR
GROUP 33D
TBD
FC OPTIMIZED:
T: 32400 FC
OR
106000 FH
533042-09-1
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
SPLICING INTO FR 40 FORWARD FITTING AND REAR FITTING
AT STR 21, LH/RH.
I:
7200 FC
OR
23800 FH
T:
18 YE
NOTE
I:
NOTE
MRB FMP
533100-270-829
1
1
MRB REFERENCE:
533042-09-1
0.86 A330-200
0.86 PRE 49202
OR
A330-300
PRE 49202
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
STRUCTURE : FUSELAGE
*
REV. DATE: JUL 01/21
SECTION:
3 -53
TBD
PAGE 99
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533051-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
147 CENTER FUSELAGE
NDT SDI
148
SPECIAL DETAILED INSPECTION (US) OF STRAP AT STR 31
LONGITUDINAL JUNCTION BETWEEN FR 53.1 AND FR 53.2.
ACCESS: 734
753
744
754
FH OPTIMIZED:
T: 29800 FC
OR
180000 FH
SOURCE
ALI
REFERENCE
533100-270-861
MEN
M/H
APPLICABILITY
1
1
0.25 GROUP 33A
0.25
*
*
0.30
0.20
1
1
0.25 GROUP
0.25 OR
GROUP
OR
GROUP
0.30 OR
0.20 GROUP
32A
TBD GROUP
OR
GROUP
OR
GROUP
OR
GROUP
32A
ALI REFERENCE:
533051-02-01
I: 13600 FC
OR
92600 FH
FC OPTIMIZED:
T: 31000 FC
OR
101400 FH
I: 14200 FC
OR
46600 FH
533051-02-2
147 CENTER FUSELAGE
NDT SDI
148
SPECIAL DETAILED INSPECTION (US) OF STRAP AT STR 31
LONGITUDINAL JUNCTION BETWEEN FR 53.1 AND FR 53.2.
ACCESS: 734
753
744
754
FH OPTIMIZED:
T: 33500 FC
OR
180000 FH
ALI
533100-270-861
ALI REFERENCE:
533051-02-02
I: 15000 FC
OR
98000 FH
*
*
33B
33C
33D
FC OPTIMIZED:
T: 34800 FC
OR
113900 FH
I: 15800 FC
OR
51600 FH
N
533052-09-1
200 CENTER FUSELAGE
NDT
SPECIAL DETAILED INSPECTION (US) OF MAIN LONGERON
EXTENSION BETWEEN FR 53.2 AND FR 53.3, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
SDI
T:
18 YE
NOTE
I:
6 YE
NOTE
MRB FMP
533100-280-823
MRB REFERENCE:
533052-09-1
1
33A
33B
33C
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 100
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533052-09-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
OR
GROUP 33D
533054-09-1
147 CENTER FUSELAGE
NDT SDI
148
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, TEE AT JUNCTION WITH FR 53.2 BULKHEAD FROM
STR 39 TO STR 43, FORWARD FACE, LH/RH.
T:
18 YE
NOTE
I:
6 YE
NOTE
MRB FMP
533100-270-842
1
1
0.55 A330-200
0.55 PRE 49202
OR
A330-300
PRE 49202
*
*
0.30
0.20
1
1
1.60 GROUP 33A
1.60 PRE 43441
(53-3039)
OR
GROUP 33C
OR
TBD GROUP 33D
OR
GROUP 33E
MRB REFERENCE:
533054-09-1
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
ACCESS: 734
753
533060-01-1
744
754
145 CENTER FUSELAGE
NDT SDI
146
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
INTERNAL STRUCTURE, FRAMES TO CROSSBEAM SPLICING AREA
AT FR 53.3 AND FR 53.5, LH/RH.
FH OPTIMIZED:
T: 19400 FC
OR
131500 FH
I:
PREP.: BOLTS;
FLOOR PANELS Z145;
FLOOR PANELS Z146;
ALI
533100-250-870
ALI REFERENCE:
533060-01-01
3000 FC
OR
20400 FH
*
FC OPTIMIZED:
T: 21600 FC
OR
70500 FH
I:
533060-01-2
145 CENTER FUSELAGE
NDT SDI
146
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
INTERNAL STRUCTURE, FRAMES TO CROSSBEAM SPLICING AREA
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
3300 FC
OR
10900 FH
FH OPTIMIZED:
T: 24800 FC
OR
168200 FH
ALI
533100-250-870
ALI REFERENCE:
533060-01-02
1
1
1.60 GROUP 33B
1.60
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 101
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533060-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.51
1
1
1.60 A330-200
1.60
* * * * *
FROM FR 53.3 TO FR 54, LH/RH.
I:
PREP.: ACT IF INSTALLED;
AIR CONDITION DUCTS;
BOLTS;
FLOOR PANELS Z145;
FLOOR PANELS Z146;
INSULATION Z140;
LDMCR (IF INSTALLED);
FC OPTIMIZED:
T: 27600 FC
OR
90300 FH
I:
533060-01-3
3600 FC
OR
24900 FH
145 CENTER FUSELAGE
NDT SDI
146
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
INTERNAL STRUCTURE, FRAMES TO CROSSBEAM SPLICING AREA
AT FR 53.3 AND FR 53.5, LH/RH.
4000 FC
OR
13300 FH
FH OPTIMIZED:
T: 21700 FC
OR
141300 FH
I:
PREP.: BOLTS;
FLOOR PANELS Z145;
FLOOR PANELS Z146;
ALI
533100-250-870
ALI REFERENCE:
533060-01-03
3200 FC
OR
20900 FH
*
TBD
FC OPTIMIZED:
T: 24000 FC
OR
84000 FH
I:
533065-01-1
151 CENTER FUSELAGE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
ATTACHMENT FITTING OF ROD LINK BETWEEN CROSS BEAM
FLOOR AND FRAME AT FR 53.3 TO FR 54, LH/RH.
3500 FC
OR
12400 FH
T: 31200 FC
I:
ALI WFD
5100 FC
533100-270-840
STRUCTURE : FUSELAGE
C O N T I N U E D
1.33 GROUP 33A
1.33
ALI REFERENCE:
533065-01-01
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z150;
* * * * *
1
1
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 102
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533065-01-1
533065-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
151 CENTER FUSELAGE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
ATTACHMENT FITTING OF ROD LINK BETWEEN CROSS BEAM
FLOOR AND FRAME AT FR 53.3 TO FR 54, LH/RH.
T: 27500 FC
I:
ALI WFD
5300 FC
533100-270-840
151 CENTER FUSELAGE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
ATTACHMENT FITTING OF ROD LINK BETWEEN CROSS BEAM
FLOOR AND FRAME AT FR 53.3 TO FR 54, LH/RH.
151 CENTER FUSELAGE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
ATTACHMENT FITTING OF ROD LINK BETWEEN CROSS BEAM
FLOOR AND FRAME AT FR 53.3 TO FR 54, LH/RH.
*
T: 29600 FC
I:
ALI WFD
5500 FC
533100-270-840
153 CENTER FUSELAGE
NDT SDI
154
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
LOWER FRAME - LATERAL FRAME SPLICING WITH CORNER
FITTING SPLICING FR 53.3 TO 54, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
C O N T I N U E D
1
1
*
T: 26300 FC
I:
ALI WFD
5200 FC
533100-270-840
ALI REFERENCE:
533065-01-04
1
1
*
T: 19200 FC
1.33 GROUP 33B
1.33 PRE 204462
(53-3250)
OR
GROUP 33C
PRE 204462
(53-3250)
TBD OR
GROUP 33D
PRE 204462
(53-3250)
1.33 GROUP 32A
1.33
ALI REFERENCE:
533065-01-03
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z150;
533066-01-1
1
1
ALI REFERENCE:
533065-01-02
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z150;
533065-01-4
M/H
* * * * *
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z150;
533065-01-3
MEN
ALI WFD
I: 10600 FC
533100-270-836
ALI REFERENCE:
533066-01-01
1
1
TBD
1.33 GROUP 32E
1.33 OR
GROUP 33E
TBD
0.93 GROUP 33A
0.93 PRE 204461
(53-3238)
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 103
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533066-01-1
533066-01-2
533066-01-3
STRUCTURE : FUSELAGE
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
MEN
M/H
PREP.: ACT IF INSTALLED;
INSULATION TO BE DISPLACED AS REQUIRED;
LDMCR;
SIDEWALL PANELS Z150;
*
6.00
ACCESS: 822
*
0.10
1
1
0.93 GROUP 33B
0.93 PRE 204461
(53-3238)
OR
GROUP 33C
PRE 204461
(53-3238)
6.00 OR
GROUP 33D
PRE 204461
(53-3238)
OR
0.10 GROUP 32E
OR
GROUP 33E
* * * * *
C O N T I N U E
SOURCE
REFERENCE
APPLICABILITY
* * * * *
153 CENTER FUSELAGE
NDT SDI
154
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
LOWER FRAME - LATERAL FRAME SPLICING WITH CORNER
FITTING SPLICING FR 53.3 TO 54, LH/RH.
T: 23100 FC
ALI WFD
I: 12500 FC
533100-270-836
ALI REFERENCE:
533066-01-02
PREP.: ACT IF INSTALLED;
INSULATION TO BE DISPLACED AS REQUIRED;
LDMCR;
SIDEWALL PANELS Z150;
*
ACCESS: 822
*
153 CENTER FUSELAGE
NDT SDI
154
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, AFTWARD LOWER SHELL, FASTENERS HOLES AT
LOWER FRAME - LATERAL FRAME SPLICING WITH CORNER
FITTING SPLICING FR 53.3 TO 54, LH/RH.
T: 25600 FC
ALI WFD
1
1
0.93 GROUP 32A
0.93 PRE 204461
(53-3238)
PREP.: ACT IF INSTALLED;
INSULATION TO BE DISPLACED AS REQUIRED;
LDMCR;
SIDEWALL PANELS Z150;
*
6.00
ACCESS: 822
*
0.10
I: 13600 FC
REV. DATE: JUL 01/21
533100-270-836
ALI REFERENCE:
533066-01-03
SECTION:
3 -53
PAGE 104
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533070-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
143 CENTER FUSELAGE
NDT SDI
149
193 SPECIAL DETAILED INSPECTION (US) OF KEEL BEAM
JUNCTION WITH CENTER WING BOX, BETWEEN FR 44 AND FR
46, Y+/-963.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
FH OPTIMIZED:
T: 35700 FC
OR
180000 FH
SOURCE
ALI
REFERENCE
533100-270-847
ALI REFERENCE:
533070-01-01
MEN
M/H
APPLICABILITY
1
1
1
0.48 GROUP 33A
0.48
0.48
1
1
1
0.48 GROUP 33C
0.48 OR
0.48 GROUP 33D
OR
GROUP 33E
1
1
1
0.48 A330-200
0.48
0.48
I: 15500 FC
OR
93400 FH
FC OPTIMIZED:
T: 40200 FC
OR
120600 FH
I: 16900 FC
OR
50800 FH
533070-01-2
143 CENTER FUSELAGE
NDT SDI
149
193 SPECIAL DETAILED INSPECTION (US) OF KEEL BEAM
JUNCTION WITH CENTER WING BOX, BETWEEN FR 44 AND FR
46, Y+/-963.
FH OPTIMIZED:
T: 27900 FC
OR
167600 FH
ALI
533100-270-847
ALI REFERENCE:
533070-01-02
I: 11700 FC
OR
70400 FH
FC OPTIMIZED:
T: 31400 FC
OR
94200 FH
I: 12700 FC
OR
38300 FH
533070-01-3
143 CENTER FUSELAGE
NDT SDI
149
193 SPECIAL DETAILED INSPECTION (US) OF KEEL BEAM
JUNCTION WITH CENTER WING BOX, BETWEEN FR 44 AND FR
46, Y+/-963.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 25000 FC
OR
162900 FH
ALI
533100-270-847
ALI REFERENCE:
533070-01-03
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 105
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533070-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 11400 FC
OR
74600 FH
FC OPTIMIZED:
T: 30300 FC
OR
106100 FH
I: 13200 FC
OR
46300 FH
533070-01-4
143 CENTER FUSELAGE
NDT SDI
149
193 SPECIAL DETAILED INSPECTION (US) OF KEEL BEAM
JUNCTION WITH CENTER WING BOX, BETWEEN FR 44 AND FR
46, Y+/-963.
FH OPTIMIZED:
T: 25900 FC
OR
155800 FH
ALI
533100-270-847
ALI REFERENCE:
533070-01-04
1
1
1
0.48 A330-900
0.48
0.48
1
1
1.10 GROUP 33A
1.10
I: 25900 FC
OR
155800 FH
FC OPTIMIZED:
T: 28400 FC
OR
85300 FH
I: 28400 FC
OR
85300 FH
533071-01-1
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF UPPER FR 48 UP TO
53.1 AT SEAT RAIL ATTACHEMENT, LH/RH.
PREP.: SIDEWALL PANELS Z250;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 43700 FC
OR
295800 FH
I:
ALI WFD
533100-270-863
ALI REFERENCE:
533071-01-01
5000 FC
OR
34300 FH
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 106
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533071-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 48600 FC
OR
158800 FH
I:
R
533072-02-1
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US + ROTOTEST) OF
FUSELAGE SKIN PANEL AT JUNCTION WITH WINDOW FRAMES,
INTERNAL ACCES FR 38 TO 53.3 AND FROM STR 18 TO 22,
LH/RH.
NOTE:
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
TASK 533072-01-1 PRIOR TO ALS PART 2 REVISION 02
PUBLICATION
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
SIDEWALL PANELS Z250;
ACCESS: 835
R
533072-02-2
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US + ROTOTEST) OF
FUSELAGE SKIN PANEL AT JUNCTION WITH WINDOW FRAMES,
INTERNAL ACCES FR 38 TO 53.3 AND FROM STR 18 TO 22,
LH/RH.
NOTE:
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
TASK 533072-01-2 PRIOR TO ALS PART 2 REVISION 02
PUBLICATION
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
5600 FC
OR
18400 FH
FH OPTIMIZED:
T: 24000 FC
OR
162700 FH
ALI
533100-270-865
ALI REFERENCE:
533072-02-01
1
1
2.56 GROUP 33A
2.56 OR
GROUP 33B
I: 10900 FC
OR
74000 FH
FC OPTIMIZED:
T: 38300 FC
OR
115100 FH
*
TBD
I: 14500 FC
OR
47400 FH
*
0.02
1
1
2.56 GROUP 33C
2.56 OR
GROUP 33D
FH OPTIMIZED:
T: 20500 FC
OR
138800 FH
I:
ALI
533100-270-865
ALI REFERENCE:
533072-02-02
9500 FC
OR
64500 FH
FC OPTIMIZED:
T: 32700 FC
OR
98200 FH
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 107
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533072-02-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
I: 12600 FC
OR
41400 FH
ACCESS: 835
533072-02-3
REFERENCE
MEN
M/H
APPLICABILITY
*
0.02
1
1
2.56 A330-900
2.56
* * * * *
SIDEWALL PANELS Z250;
R
SOURCE
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US + ROTOTEST) OF
FUSELAGE SKIN PANEL AT JUNCTION WITH WINDOW FRAMES,
INTERNAL ACCES FR 38 TO 53.3 AND FROM STR 18 TO 22,
LH/RH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
SIDEWALL PANELS Z250;
ACCESS: 835
FH OPTIMIZED:
T: 26000 FC
OR
156400 FH
ALI
533100-270-865
ALI REFERENCE:
533072-02-03
I: 11400 FC
OR
77700 FH
FC OPTIMIZED:
T: 27400 FC
OR
82400 FH
*
TBD
*
0.02
1
1
2.50 A330-200F
2.50
I: 12000 FC
OR
36100 FH
533075-01-1
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
INTERNAL STRUCTURE, FRAME SPLICINGS 39 TO 39.2 AT STR
20-23, RH/LH.
PREP.: BOLTS;
INSULATION TO BE DISPLACED AS REQUIRED;
SIDEWALL PANELS Z250;
T: 33000 FC
OR
100000 FH
I:
ALI
533100-250-877
ALI REFERENCE:
533075-01-01
3700 FC
OR
11700 FH
ACCESS: 835
533078-01-1
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
STRINGER SPLICING FLANGE AREA AT CIRCUMFERENTIAL
JUNCTION AT FR 54, FROM STR 3 LH TO STR 3 RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 14500 FC
OR
87200 FH
ALI
533100-220-950
*
TBD
*
0.02
1
1
0.03 A330-900
0.03 PRE 204887
ALI REFERENCE:
533078-01-01
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 108
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533078-01-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
I: 10400 FC
OR
62700 FH
*
TBD
FC OPTIMIZED:
T: 17000 FC
OR
50000 FH
I: 11600 FC
OR
34800 FH
533078-01-2
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
STRINGER SPLICING FLANGE AREA AT CIRCUMFERENTIAL
JUNCTION AT FR 54, FROM STR 3 LH TO STR 3 RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
FH OPTIMIZED:
T: 18100 FC
OR
109100 FH
ALI
533100-220-950
1
1
0.03 A330-900
0.03 POST 204887
ALI REFERENCE:
533078-01-02
I: 13500 FC
OR
81400 FH
*
TBD
1
1
TBD A330-800
TBD PRE 204887
*
TBD
FC OPTIMIZED:
T: 20700 FC
OR
62200 FH
I: 15000 FC
OR
45200 FH
N
533078-01-3
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
STRINGER SPLICING FLANGE AREA AT CIRCUMFERENTIAL
JUNCTION AT FR 54, FROM STR 3 LH TO STR 3 RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 16900 FC
OR
110000 FH
ALI
533100-220-950
ALI REFERENCE:
533078-01-03
I: 12300 FC
OR
79900 FH
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 109
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533078-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 20200 FC
OR
71000 FH
I: 13800 FC
OR
48600 FH
N
533078-01-4
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
STRINGER SPLICING FLANGE AREA AT CIRCUMFERENTIAL
JUNCTION AT FR 54, FROM STR 3 LH TO STR 3 RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z250;
FH OPTIMIZED:
T: 21100 FC
OR
137300 FH
ALI
533100-220-950
ALI REFERENCE:
533078-01-04
I: 16100 FC
OR
104700 FH
1
1
TBD A330-800
TBD POST 204887
*
TBD
FC OPTIMIZED:
T: 25300 FC
OR
88600 FH
I: 18100 FC
OR
63600 FH
R
533080-01-1
250 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTOTEST) OF FUSELAGE
CIRCUMFERENTIAL JOINT AT FR 53.3 FROM STR 13 TO STR
16, EXTERNAL SURFACE, LH/RH.
PREP.: BOLTS;
533103-02-1
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
SKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR 19,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
T: 17000 FC
OR
51000 FH
ALI
533100-250-892
ALI REFERENCE:
533080-01-01
I: 17000 FC
OR
51000 FH
FH OPTIMIZED:
T: 12400 FC
OR
84100 FH
1
*
ALI
533100-220-817
1
2.40 A330-800
OR
A330-900
PRE 207464
OR
A330-900
TBD PRE 207465
0.20 GROUP 33A
PRE 45749 S13894
ALI REFERENCE:
533103-02-01
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 110
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533103-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
6200 FC
OR
42100 FH
FC OPTIMIZED:
T: 13800 FC
OR
45100 FH
I:
533103-02-2
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
SKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR 19,
LH/RH.
6900 FC
OR
22500 FH
FH OPTIMIZED:
T: 29000 FC
OR
190400 FH
I:
NOTE:
FOR AIRCRAFT POST 45749 THRESHOLD IS TO BE COUNTED
FROM SB 53-3091 EMBODIMENT.
ALI
533100-220-817
1
0.20 GROUP 32A
OR
GROUP 33A
POST 45749 S13894
OR
GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
1
0.20 A330-200F
ALI REFERENCE:
533103-02-02
5000 FC
OR
34200 FH
FC OPTIMIZED:
T: 32300 FC
OR
105600 FH
I:
533103-02-3
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
SKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR 19,
LH/RH.
STRUCTURE : FUSELAGE
5600 FC
OR
18300 FH
T: 31600 FC
OR
94900 FH
I:
ALI
533100-220-817
ALI REFERENCE:
533103-02-03
7300 FC
OR
22400 FH
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 111
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533104-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND
ANTI-COLLISION LIGHT CUTOUT BETWEEN FR 42 AND FR 43,
BETWEEN STR 1 LH AND STR 1 RH.
FH OPTIMIZED:
T: 34900 FC
OR
180000 FH
I:
PREP.: ANTENNA;
ANTICOLLISION LIGHTS;
OBTURATORS WHERE INSTALLED;
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND
ANTI-COLLISION LIGHT CUTOUT BETWEEN FR 42 AND FR 43,
BETWEEN STR 1 LH AND STR 1 RH.
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND
ANTI-COLLISION LIGHT CUTOUT BETWEEN FR 42 AND FR 43,
BETWEEN STR 1 LH AND STR 1 RH.
1
0.20 GROUP 33A
OR
GROUP 33B
*
0.40
1
0.25 GROUP 33C
PRE 48829
OR
GROUP 33D
PRE 48829
*
0.40
1
0.25 GROUP 33C
POST 48829
OR
GROUP 33D
POST 48829
*
0.40
ALI REFERENCE:
533104-01-03
ALI
533100-220-815
ALI REFERENCE:
533104-01-04
1700 FC
1700 FC
ALI
533100-220-815
ALI REFERENCE:
533104-01-05
2000 FC
FC OPTIMIZED:
T: 37200 FC
OR
111800 FH
I:
STRUCTURE : FUSELAGE
APPLICABILITY
1800 FC
FH OPTIMIZED:
T: 33300 FC
OR
180000 FH
I:
PREP.: ANTENNA;
ANTICOLLISION LIGHTS;
OBTURATORS WHERE INSTALLED;
M/H
FC OPTIMIZED:
T: 33400 FC
OR
100400 FH
I:
200 CENTER FUSELAGE
533100-220-815
MEN
1800 FC
FH OPTIMIZED:
T: 29900 FC
OR
180000 FH
I:
PREP.: ANTENNA;
ANTICOLLISION LIGHTS;
OBTURATORS WHERE INSTALLED;
533104-01-7
ALI
REFERENCE
FC OPTIMIZED:
T: 39100 FC
OR
117400 FH
I:
533104-01-6
SOURCE
2000 FC
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 112
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
FH OPTIMIZED:
T: 23800 FC
OR
161400 FH
I:
SOURCE
ALI
REFERENCE
533100-220-850
MEN
M/H
APPLICABILITY
1
2.00 GROUP 32A
OR
GROUP 33A
OR
GROUP 33B
1
2.00 GROUP 33E
1
2.00 GROUP 32E
ALI REFERENCE:
533106-01-02
5900 FC
OR
39900 FH
FC OPTIMIZED:
T: 38100 FC
OR
114300 FH
I:
533106-01-4
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
7800 FC
OR
25600 FH
FH OPTIMIZED:
T: 13400 FC
OR
91100 FH
I:
ALI
533100-220-850
ALI REFERENCE:
533106-01-05
4100 FC
OR
27700 FH
FC OPTIMIZED:
T: 21400 FC
OR
64400 FH
I:
533106-01-5
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
5400 FC
OR
17800 FH
FH OPTIMIZED:
T: 17500 FC
OR
118800 FH
ALI
533100-220-850
ALI REFERENCE:
533106-01-06
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 113
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-01-5
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
5000 FC
OR
33800 FH
FC OPTIMIZED:
T: 27600 FC
OR
96900 FH
I:
533106-01-6
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
6500 FC
OR
23000 FH
FH OPTIMIZED:
T: 20300 FC
OR
137800 FH
I:
ALI
533100-220-850
1
2.00 GROUP 33C
OR
GROUP 33D
1
2.00 A330-900
ALI REFERENCE:
533106-01-04
5100 FC
OR
34800 FH
FC OPTIMIZED:
T: 32500 FC
OR
97500 FH
I:
533106-01-7
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
6800 FC
OR
22300 FH
FH OPTIMIZED:
T: 15700 FC
OR
94500 FH
I:
ALI
533100-220-850
ALI REFERENCE:
533106-01-07
4400 FC
OR
26400 FH
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 114
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 17900 FC
OR
53900 FH
I:
N
533106-01-8
200 CENTER FUSELAGE
AF
DET
DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE,
FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE
SKIN BETWEEN STR 18 AND STR 22, FROM FR 38 TO 53.3,
LH/RH.
4800 FC
OR
14600 FH
FH OPTIMIZED:
T: 17600 FC
OR
115000 FH
I:
ALI
533100-220-850
1
TBD A330-800
1
5.87 GROUP 32A
OR
GROUP 33A
OR
GROUP 33B
ALI REFERENCE:
533106-01-08
5000 FC
OR
32800 FH
FC OPTIMIZED:
T: 21200 FC
OR
74200 FH
I:
533106-02-1
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
5700 FC
OR
19900 FH
FH OPTIMIZED:
T: 16400 FC
OR
111600 FH
I:
ALI
533100-250-864
ALI REFERENCE:
533106-02-01
5000 FC
OR
34200 FH
FC OPTIMIZED:
T: 26300 FC
OR
79000 FH
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 115
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
200 CENTER FUSELAGE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I:
533106-02-2
SOURCE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
6700 FC
OR
21900 FH
FH OPTIMIZED:
T: 13600 FC
OR
92000 FH
I:
ALI
533100-250-864
1
5.87 GROUP 33C
OR
GROUP 33D
1
5.87 GROUP 33E
ALI REFERENCE:
533106-02-02
4300 FC
OR
29200 FH
FC OPTIMIZED:
T: 21700 FC
OR
65100 FH
I:
533106-02-3
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
5700 FC
OR
18700 FH
FH OPTIMIZED:
T: 13400 FC
OR
91100 FH
I:
ALI
533100-250-864
ALI REFERENCE:
533106-02-03
4100 FC
OR
27700 FH
FC OPTIMIZED:
T: 21400 FC
OR
64400 FH
I:
STRUCTURE : FUSELAGE
5400 FC
OR
17800 FH
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 116
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-02-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
FH OPTIMIZED:
T: 17500 FC
OR
118800 FH
I:
SOURCE
ALI
REFERENCE
533100-250-864
MEN
M/H
APPLICABILITY
1
5.87 GROUP 32E
1
5.87 A330-900
1
TBD A330-800
ALI REFERENCE:
533106-02-04
5000 FC
OR
33800 FH
FC OPTIMIZED:
T: 27600 FC
OR
96900 FH
I:
533106-02-5
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
6500 FC
OR
23000 FH
FH OPTIMIZED:
T: 15700 FC
OR
94500 FH
I:
ALI
533100-250-864
ALI REFERENCE:
533106-02-05
4400 FC
OR
26400 FH
FC OPTIMIZED:
T: 17900 FC
OR
53900 FH
I:
N
533106-02-6
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES
JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22,
FROM FR 38 TO 53.3, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
4800 FC
OR
14600 FH
FH OPTIMIZED:
T: 17600 FC
OR
115000 FH
ALI
533100-250-864
ALI REFERENCE:
533106-02-06
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 117
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533106-02-6
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
1
1
1
1
0.45
0.45
0.45
0.45
FC OPTIMIZED:
T: 25300 FC
OR
82900 FH
*
1.00
I: 10600 FC
OR
34900 FH
*
*
0.30
0.15
1
1
1
1
0.45
0.45
0.45
0.45
APPLICABILITY
* * * * *
I:
5000 FC
OR
32800 FH
FC OPTIMIZED:
T: 21200 FC
OR
74200 FH
I:
R
533107-01-3
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US & ROTOTEST) OF
138 FUSELAGE INTERNAL STRUCTURE, FR 39 TO 39.2, WEB HOLE
AREA JUST BELOW STR 28 AND FASTENERS AREA AT FRAMES
JUNCTION BELOW STR 29 LEVEL, LH/RH.
NOTE:
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
TASK 533107-01-10 PRIOR TO ALS PART 2 REVISION 02
PUBLICATION
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
BOLTS;
ACCESS: 131BX
132CX
533107-01-4
131CX
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US & ROTOTEST) OF
138 FUSELAGE INTERNAL STRUCTURE, FR 39 TO 39.2, WEB HOLE
AREA JUST BELOW STR 28 AND FASTENERS AREA AT FRAMES
JUNCTION BELOW STR 29 LEVEL, LH/RH.
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
BOLTS;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
5700 FC
OR
19900 FH
FH OPTIMIZED:
T: 22800 FC
OR
154500 FH
I:
533100-200-852
ALI REFERENCE:
533107-01-03
9600 FC
OR
65200 FH
FH OPTIMIZED:
T: 19700 FC
OR
133700 FH
I:
ALI WFD
ALI
533100-200-852
ALI REFERENCE:
533107-01-04
9400 FC
OR
62400 FH
*
GROUP 33A
OR
GROUP 33C
POST 49202
OR
GROUP 33D
POST 49202
GROUP 32A
PRE 49202
OR
GROUP 33B
OR
GROUP 33C
PRE 49202
1.00 OR
GROUP 33D
PRE 49202
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 118
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533107-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
ACCESS: 131BX
132CX
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.30
0.15
1
1
1
1
0.45 GROUP 33E
0.45
0.45
0.45
*
1.00
*
*
0.30
0.15
1
1
1
1
0.45 GROUP 32E
0.45
0.45
0.45
*
1.00
*
*
0.30
0.15
* * * * *
131CX
FC OPTIMIZED:
T: 21900 FC
OR
71700 FH
I: 10400 FC
OR
34200 FH
533107-01-6
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US & ROTOTEST) OF
138 FUSELAGE INTERNAL STRUCTURE, FR 39 TO 39.2, WEB HOLE
AREA JUST BELOW STR 28 AND FASTENERS AREA AT FRAMES
JUNCTION BELOW STR 29 LEVEL, LH/RH.
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
BOLTS;
ACCESS: 131BX
132CX
131CX
FH OPTIMIZED:
T: 24200 FC
OR
164200 FH
I:
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US & ROTOTEST) OF
138 FUSELAGE INTERNAL STRUCTURE, FR 39 TO 39.2, WEB HOLE
AREA JUST BELOW STR 28 AND FASTENERS AREA AT FRAMES
JUNCTION BELOW STR 29 LEVEL, LH/RH.
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
BOLTS;
ACCESS: 131BX
132CX
* * * * *
STRUCTURE : FUSELAGE
131CX
C O N T I N U E D
533100-200-852
ALI REFERENCE:
533107-01-06
8200 FC
OR
55600 FH
FC OPTIMIZED:
T: 26900 FC
OR
88100 FH
I:
533107-01-7
ALI WFD
9100 FC
OR
29700 FH
FH OPTIMIZED:
T: 26100 FC
OR
170000 FH
I:
ALI WFD
533100-200-852
ALI REFERENCE:
533107-01-07
8300 FC
OR
54000 FH
FC OPTIMIZED:
T: 28800 FC
OR
101000 FH
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 119
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533107-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US & ROTOTEST) OF
138 FUSELAGE INTERNAL STRUCTURE, FR 39 TO 39.2, WEB HOLE
AREA JUST BELOW STR 28 AND FASTENERS AREA AT FRAMES
JUNCTION BELOW STR 29 LEVEL, LH/RH.
MEN
M/H
APPLICABILITY
9100 FC
OR
32100 FH
FH OPTIMIZED:
T: 24500 FC
OR
159300 FH
I:
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
BOLTS;
ACCESS: 131BX
132CX
REFERENCE
* * * * *
I:
533107-01-9
SOURCE
ALI WFD
533100-200-852
ALI REFERENCE:
533107-01-09
9600 FC
OR
62400 FH
FC OPTIMIZED:
T: 27000 FC
OR
94600 FH
131CX
1
1
1
1
0.45 GROUP 32A
0.45 POST 49202
0.45
0.45
*
1.00
*
*
0.30
0.15
1
1
1
1
1.07 A330-900
1.07 PRE 207401
1.07
1.07
*
1.00
I: 10600 FC
OR
37100 FH
R
533107-02-2
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
138 STRUCTURE, FR 39 TO 39.2 WEB HOLE AREA JUST BELOW STR
28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STR 29
LEVEL, LH/RH.
T: 23300 FC
I:
ALI WFD
9000 FC
533100-270-870
ALI REFERENCE:
533107-02-02
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z130;
N
533107-02-3
131 CENTER FUSELAGE
NDT SDI
132
137 SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
138 STRUCTURE, FR 39 TO 39.2 WEB HOLE AREA JUST BELOW STR
28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STR 29
LEVEL, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
T: 30500 FC
ALI WFD
I: 11300 FC
533100-270-870
ALI REFERENCE:
533107-02-03
1
1
1
1
TBD A330-800
TBD
TBD
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 120
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533107-02-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
100 MAIN STRUCTURE
M/H
APPLICABILITY
*
1.00
1
0.54 GROUP 32A
PRE 49202
OR
GROUP 33B
OR
GROUP 33C
PRE 49202
OR
GROUP 33D
PRE 49202
1
0.54 GROUP 33A
* * * * *
PREP.: AIR CONDITIONING DUCTS IN Z137/138;
INSULATION TO BE DISPLACED AS REQUIRED;
LINING Z130;
533112-01-2
MEN
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, LONGITUDINAL JOINT AT STR 39 AHEAD OF FR
53.2, LH/RH.
FH OPTIMIZED:
T: 36500 FC
OR
237800 FH
ALI
533100-270-825
ALI REFERENCE:
533112-01-02
I: 32100 FC
OR
208800 FH
FC OPTIMIZED:
T: 38300 FC
OR
125400 FH
I: 33900 FC
OR
111000 FH
533112-01-3
100 MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, LONGITUDINAL JOINT AT STR 39 AHEAD OF FR
53.2, LH/RH.
FH OPTIMIZED:
T: 39000 FC
OR
180000 FH
ALI
533100-270-825
ALI REFERENCE:
533112-01-01
I: 32700 FC
OR
180000 FH
FC OPTIMIZED:
T: 40600 FC
OR
132600 FH
I: 34100 FC
OR
111500 FH
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 121
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533113-01-4
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
FH OPTIMIZED:
T: 4500 FC
OR
30800 FH
I:
SOURCE
ALI
REFERENCE
533100-200-854
MEN
M/H
APPLICABILITY
1
0.75 GROUP 33A
1
0.75 GROUP 33C
OR
GROUP 33D
OR
GROUP 33E
1
0.75 GROUP 32E
ALI REFERENCE:
533113-01-04
4500 FC
OR
30800 FH
FC OPTIMIZED:
T: 7200 FC
OR
21800 FH
I:
533113-01-5
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
6700 FC
OR
21800 FH
FH OPTIMIZED:
T: 14100 FC
OR
95900 FH
ALI
533100-200-854
ALI REFERENCE:
533113-01-05
I: 11100 FC
OR
75400 FH
FC OPTIMIZED:
T: 22600 FC
OR
67900 FH
I: 14800 FC
OR
48300 FH
533113-01-6
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 18500 FC
OR
125600 FH
ALI
533100-200-854
ALI REFERENCE:
533113-01-06
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 122
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533113-01-6
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 13500 FC
OR
91900 FH
FC OPTIMIZED:
T: 29200 FC
OR
102500 FH
I: 17900 FC
OR
62600 FH
533113-01-8
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
FH OPTIMIZED:
T: 18500 FC
OR
125600 FH
ALI
533100-200-854
1
0.75 GROUP 32A
1
0.75 A330-200F
ALI REFERENCE:
533113-01-06
I: 13500 FC
OR
91900 FH
FC OPTIMIZED:
T: 29200 FC
OR
102500 FH
I: 17900 FC
OR
62600 FH
533113-01-10
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
STRUCTURE : FUSELAGE
T: 11900 FC
I:
ALI
533100-200-854
7770 FC
ALI REFERENCE:
533113-01-10
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 123
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533113-01-11
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
FH OPTIMIZED:
T: 5500 FC
OR
37300 FH
I:
SOURCE
ALI
REFERENCE
533100-200-854
MEN
M/H
APPLICABILITY
1
0.75 GROUP 33B
PRE 43720
1
0.75 GROUP 33B
POST 43720
1
1
0.27 GROUP 33A
0.27
ALI REFERENCE:
533113-01-11
4800 FC
OR
33000 FH
FC OPTIMIZED:
T: 8800 FC
OR
26400 FH
I:
533113-01-12
200 CENTER FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE EXTERNAL
STRUCTURE, FASTENERS ROWS AT FR 47, FROM BELOW STR 22
TO ABOVE STR 24 LEVEL, LH/RH.
6400 FC
OR
21100 FH
FH OPTIMIZED:
T: 15400 FC
OR
104600 FH
ALI
533100-200-854
ALI REFERENCE:
533113-01-12
I: 12400 FC
OR
84400 FH
FC OPTIMIZED:
T: 24600 FC
OR
74000 FH
I: 16500 FC
OR
54100 FH
533114-01-3
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
FH OPTIMIZED:
T: 13400 FC
OR
91200 FH
ALI
533100-200-846
ALI REFERENCE:
533114-01-03
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
*
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 124
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533114-01-3
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.10
0.10
1
1
0.27 GROUP 32A
0.27 PRE 49202
OR
GROUP 33B
POST 43720
OR
TBD GROUP 33C
PRE 49202
0.10 OR
0.10 GROUP 33D
PRE 49202
* * * * *
I: 13000 FC
OR
88100 FH
ACCESS: 251XW
252XW
FC OPTIMIZED:
T: 21500 FC
OR
64600 FH
I: 17300 FC
OR
56500 FH
533114-01-4
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
FH OPTIMIZED:
T: 11100 FC
OR
75700 FH
ALI
533100-200-846
ALI REFERENCE:
533114-01-04
I: 11000 FC
OR
74500 FH
*
*
*
FC OPTIMIZED:
T: 17800 FC
OR
53600 FH
I: 14600 FC
OR
47800 FH
533114-01-7
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
FH OPTIMIZED:
T: 16600 FC
OR
112400 FH
ALI
533100-200-846
ALI REFERENCE:
533114-01-07
I: 16200 FC
OR
109700 FH
1
1
0.27 GROUP 33B
0.27 PRE 43720
*
TBD
*
*
0.10
0.10
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 125
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533114-01-7
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 26500 FC
OR
79500 FH
I: 21500 FC
OR
70300 FH
533114-01-8
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
FH OPTIMIZED:
T: 13700 FC
OR
93000 FH
ALI
533100-200-846
ALI REFERENCE:
533114-01-08
I: 11000 FC
OR
74500 FH
1
1
*
*
0.27 GROUP 32A
0.27 POST 49202
OR
GROUP 33C
POST 49202
OR
TBD GROUP 33D
POST 49202
0.10
0.10
1
1
0.27 GROUP 33E
0.27 PRE 53539
*
FC OPTIMIZED:
T: 21900 FC
OR
65800 FH
I: 14600 FC
OR
47800 FH
533114-01-9
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
* * * * *
STRUCTURE : FUSELAGE
FH OPTIMIZED:
T: 10100 FC
OR
68900 FH
I:
ALI
533100-200-846
ALI REFERENCE:
533114-01-09
7800 FC
OR
53200 FH
FC OPTIMIZED:
T: 16200 FC
OR
48700 FH
C O N T I N U E D
*
TBD
*
*
0.10
0.10
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 126
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533114-01-9
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 10400 FC
OR
34100 FH
533114-01-10
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
FH OPTIMIZED:
T: 13200 FC
OR
89600 FH
ALI
533100-200-846
1
1
0.27 GROUP 33E
0.27 POST 53539
ALI REFERENCE:
533114-01-10
I: 11600 FC
OR
78600 FH
FC OPTIMIZED:
T: 21100 FC
OR
63400 FH
*
TBD
*
*
0.10
0.10
1
1
0.27 GROUP 32E
0.27 PRE 53539
I: 15400 FC
OR
50400 FH
533114-01-11
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
FH OPTIMIZED:
T: 13300 FC
OR
90200 FH
I:
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
ALI
533100-200-846
ALI REFERENCE:
533114-01-11
9500 FC
OR
64800 FH
FC OPTIMIZED:
T: 21000 FC
OR
73600 FH
*
TBD
*
*
0.10
0.10
I: 12600 FC
OR
44200 FH
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 127
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533114-01-12
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
251 CENTER FUSELAGE
NDT SDI
252
SPECIAL DETAILED INSPECTION (US) OF FUSELAGE INTERNAL
STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERS AT
STR 20 TO 23, LH/RH.
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
ACCESS: 251XW
252XW
FH OPTIMIZED:
T: 17300 FC
OR
117400 FH
SOURCE
ALI
REFERENCE
533100-200-846
MEN
1
1
M/H
APPLICABILITY
0.27 GROUP 32E
0.27 POST 53539
ALI REFERENCE:
533114-01-12
I: 14100 FC
OR
95800 FH
FC OPTIMIZED:
T: 27300 FC
OR
95800 FH
*
TBD
*
*
0.10
0.10
1
1
*
0.20 GROUP 32A
0.20 PRE 49202
OR
GROUP 33A
OR
TBD GROUP 33B
*
*
0.10
0.10
1
1
0.20 GROUP 33C
0.20 PRE 49202
OR
GROUP 33D
PRE 49202
TBD
I: 18600 FC
OR
65300 FH
533115-01-4
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 47 STABILIZERS FROM STR 19 TO 23, LH/RH.
FH OPTIMIZED:
T: 10000 FC
OR
67700 FH
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
I: 10000 FC
OR
67700 FH
ACCESS: 251XW
252XW
ALI
533100-220-816
ALI REFERENCE:
533115-01-04
FC OPTIMIZED:
T: 15900 FC
OR
47900 FH
I: 15200 FC
OR
47900 FH
533115-01-5
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 47 STABILIZERS FROM STR 19 TO 23, LH/RH.
FH OPTIMIZED:
T: 7700 FC
OR
52200 FH
ALI
533100-220-816
ALI REFERENCE:
533115-01-05
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
*
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 128
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533115-01-5
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
*
0.10
0.10
1
1
0.20 GROUP 33C
0.20 POST 49202
OR
GROUP 33D
POST 49202
TBD OR
GROUP 33E
0.10
0.10
* * * * *
ACCESS: 251XW
252XW
I:
7700 FC
OR
52200 FH
FC OPTIMIZED:
T: 12300 FC
OR
36900 FH
I: 11800 FC
OR
36900 FH
533115-01-6
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 47 STABILIZERS FROM STR 19 TO 23, LH/RH.
FH OPTIMIZED:
T: 14000 FC
OR
95200 FH
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
I: 14000 FC
OR
95200 FH
ACCESS: 251XW
252XW
ALI
533100-220-816
ALI REFERENCE:
533115-01-06
*
*
*
FC OPTIMIZED:
T: 22400 FC
OR
67400 FH
I: 21300 FC
OR
67400 FH
533115-01-7
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 47 STABILIZERS FROM STR 19 TO 23, LH/RH.
FH OPTIMIZED:
T: 18400 FC
OR
124700 FH
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
I: 18400 FC
OR
124700 FH
ACCESS: 251XW
252XW
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
ALI
533100-220-816
ALI REFERENCE:
533115-01-07
1
1
0.20 GROUP 32A
0.20 POST 49202
OR
GROUP 32E
*
TBD
*
*
0.10
0.10
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 129
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533115-01-7
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T: 29000 FC
OR
101800 FH
I: 25800 FC
OR
90500 FH
533115-01-9
533117-01-1
251 CENTER FUSELAGE
AF
DET
252
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
FR 47 STABILIZERS FROM STR 19 TO 23, LH/RH.
I:
ALI
8500 FC
533100-220-816
ALI REFERENCE:
533115-01-09
1
1
0.20 A330-200F
0.20
PREP.: INSULATION TO BE DISPLACED AS REQUIRED;
*
TBD
ACCESS: 251XW
252XW
*
*
0.10
0.10
1
1
1
0.30 ALL
0.30
0.30
191 FR40 BULKHEAD
AF
DET
192
193 DETAILED INSPECTION OF FR 40 PRESSURE BULKHEAD, AFT
FACE BELOW CENTER WING BOX.
TPS
533122-01-1
T: 13000 FC
T:
12 YE
I:
12 YE
MRB CPCP
533100-200-803
MRB REFERENCE:
533117-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: WATER EXTRACTOR CONDENSER REHEATER;
*
TBD
ACCESS: 191KB
192PB
193BB
*
*
*
2.00
2.00
1.00
1
1.00 ALL
149 CENTER LANDING GEAR WELL
AF
GVI
T:
6 YE
GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR
WELL, KEEL BEAM INTERNAL STRUCTURE AND PANELS BETWEEN
FR 47 AND FR 53.2.
I:
6 YE
MRB CPCP
533100-200-830
MRB REFERENCE:
533122-01-1
NOTE:
A CENTER LANDING GEAR IS NOT FITTED TO THE A330.
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 130
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533122-01-1
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
*
0.30
1
1
0.60 ALL
0.60
*
*
0.15
0.15
1
1
1
0.25 GROUP 33A
0.25
0.25
*
*
0.15
0.15
1
1
1
0.25 A330-200F
0.25
0.25
* * * * *
HOWEVER, THE TERM CENTER LANDING GEAR HAS BEEN KEPT
IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL
COMMONALITY WITH THE A340 IN THIS AREA.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
533123-01-1
744
147 MAIN LANDING GEAR BAY
AF
148
DETAILED INSPECTION OF MAIN LANDING GEAR BAY,
PRESSURE DIAPHRAGMS AND PRESSURIZED FLOORS LOWER
SURFACE, BETWEEN FR 47 AND FR 53.2.
TPS
DET
T:
6 YE
I:
6 YE
MRB CPCP
533100-200-831
MRB REFERENCE:
533123-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
533125-01-1
147 CENTER LANDING GEAR WELL
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2
PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF
THE CENTER LANDING GEAR TRUNNION FITTINGS.
T:
I:
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
TPS
6 YE
OR
3600 FC
ALI
MRB CPCP
533100-200-832
ALI REFERENCE:
533125-01-01
6 YE
OR
3600 FC
MRB REFERENCE:
533125-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
533125-01-2
147 CENTER LANDING GEAR WELL
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2
PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
T:
6 YE
OR
4500 FC
MRB
MRB CPCP
533100-200-832
MRB REFERENCE:
533125-01-1
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 131
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533125-01-2
* * * * *
C O N T I N U E
REFERENCE
I:
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
6 YE
OR
4500 FC
533125-01-3
T:
I:
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
6 YE
OR
6200 FC
ALI
MRB CPCP
533100-200-832
ALI REFERENCE:
533125-01-02
6 YE
OR
6200 FC
0.15
0.15
1
1
1
0.25 GROUP 33B
0.25 OR
0.25 GROUP 32E
POST 41652 S11927
OR
GROUP 33E
POST 41652 S11927
OR
A330-800
OR
A330-900
*
*
0.15
0.15
1
1
1
0.25 GROUP 32A
0.25 OR
0.25 GROUP 33C
OR
GROUP 33D
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
147 CENTER LANDING GEAR WELL
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2
PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF
THE CENTER LANDING GEAR TRUNNION FITTINGS.
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
* * * * *
STRUCTURE : FUSELAGE
*
*
MRB REFERENCE:
533125-01-1
ACCESS: 734
744
533125-01-4
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
147 CENTER LANDING GEAR WELL
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2
PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF
THE CENTER LANDING GEAR TRUNNION FITTINGS.
TPS
M/H
533125-01-2
ACCESS: 734
744
R
MEN
* * * * *
THE CENTER LANDING GEAR TRUNNION FITTINGS.
TPS
SOURCE
C O N T I N U E D
T:
I:
6 YE
OR
7200 FC
ALI
MRB CPCP
533100-200-832
ALI REFERENCE:
533125-01-03
6 YE
OR
7200 FC
MRB REFERENCE:
533125-01-1
REV. DATE: JUL 01/21
SECTION:
* * * * *
3-53
PAGE 132
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533125-01-4
* * * * *
TPS
C O N T I N U E
SOURCE
REFERENCE
533125-01-5
M/H
APPLICABILITY
*
*
0.15
0.15
1
1
1
0.25 GROUP 32E
0.25 PRE 41652 S11927
0.25 OR
GROUP 33E
PRE 41652 S11927
*
*
0.15
0.15
1
1
1
0.08 GROUP 33A
0.08
0.08
*
*
0.15
0.15
* * * * *
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
R
MEN
147 CENTER LANDING GEAR WELL
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2
PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF
THE CENTER LANDING GEAR TRUNNION FITTINGS.
T:
6 YE
I:
6 YE
MRB CPCP
533100-200-832
MRB REFERENCE:
533125-01-1
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
533126-01-2
147 MLG AND CLG CUTOUT
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND
CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO
AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
TPS
FH OPTIMIZED:
T:
6 YE
OR
7400 FC
OR
50200 FH
I:
MRB
MRB CPCP
533100-200-833
MRB REFERENCE:
533126-01-2
533126-01-9
6 YE
OR
7400 FC
OR
50200 FH
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
* * * * *
STRUCTURE : FUSELAGE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 133
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533126-01-2
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
FC OPTIMIZED:
T:
6 YE
OR
7700 FC
OR
25200 FH
I:
533126-01-4
147 MLG AND CLG CUTOUT
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND
CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO
AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
TPS
FH OPTIMIZED:
T:
6 YE
OR
4900 FC
OR
32000 FH
I:
MRB
MRB CPCP
533100-200-833
MRB REFERENCE:
533126-01-2
533126-01-8
1
1
1
0.08 GROUP 32A
0.08 OR
0.08 GROUP 33B
OR
GROUP 33C
OR
GROUP 33D
*
*
0.15
0.15
6 YE
OR
4900 FC
OR
32000 FH
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
FC OPTIMIZED:
T:
6 YE
OR
5200 FC
OR
17000 FH
I:
STRUCTURE : FUSELAGE
6 YE
OR
7700 FC
OR
25200 FH
6 YE
OR
5200 FC
OR
17000 FH
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 134
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533126-01-6
ZONE
DESCRIPTION
147 MLG AND CLG CUTOUT
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND
CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO
AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
TPS
FH OPTIMIZED:
T:
6 YE
OR
5200 FC
OR
34400 FH
I:
SOURCE
MRB
MRB CPCP
REFERENCE
533100-200-833
MRB REFERENCE:
533126-01-10
533126-01-2
147 MLG AND CLG CUTOUT
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND
CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO
AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
M/H
APPLICABILITY
1
1
1
0.08 GROUP 32E
0.08 OR
0.08 GROUP 33E
*
*
0.15
0.15
1
1
1
0.08 A330-200F
0.08
0.08
*
*
0.15
0.15
6 YE
OR
5200 FC
OR
34400 FH
FC OPTIMIZED:
T:
6 YE
OR
5500 FC
OR
17900 FH
I:
6 YE
OR
5500 FC
OR
17900 FH
T:
6 YE
OR
4900 FC
I:
MRB
MRB CPCP
6 YE
OR
4900 FC
533100-200-833
MRB REFERENCE:
533126-01-2
533126-01-7
ACCESS: 734
744
STRUCTURE : FUSELAGE
MEN
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
533126-01-7
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 135
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
533126-01-8
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
147 MLG AND CLG CUTOUT
AF
GVI
148
149 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND
CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO
AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.
T:
I:
NOTE:
A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE
DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY
WITH THE A340 IN THIS AREA.
6 YE
OR
5400 FC
SOURCE
MRB
MRB CPCP
REFERENCE
533100-200-833
MRB REFERENCE:
533126-01-11
533126-01-2
6 YE
OR
5400 FC
ACCESS: 734
744
533127-02-1
191
192
193
195
196
AIR CONDITIONING ACCESS CUTOUT
191KB
193BB
6 YE
I:
6 YE
MRB CPCP
533100-200-834
MRB REFERENCE:
533127-02-1
193DB
AIR CONDITIONING ACCESS CUTOUT
AF
DET
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
* * * * *
STRUCTURE : FUSELAGE
T:
M/H
APPLICABILITY
1
1
1
0.08 A330-800
0.08 OR
0.08 A330-900
*
*
0.15
0.15
1
1
1
1
1
0.05 ALL
0.05
0.05
0.05
0.05
*
*
3.70
5.10
1
1
1
1
1
0.10 GROUP 33A
0.10 OR
0.10 GROUP 33B
0.10
0.10
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 191FB
193AB
191
192
193
195
196
GVI
GENERAL VISUAL INSPECTION OF AREA AROUND
AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0
CM (6.0 IN) EXTERNAL SURFACE.
TPS
533127-03-1
AF
MEN
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
PANELS
PANELS
PANELS
PANELS
PANELS
ALI
533100-220-801
ALI REFERENCE:
533127-03-01
I: 10600 FC
OR
72100 FH
Z191;
Z192;
Z193;
Z195;
Z196;
C O N T I N U E D
FH OPTIMIZED:
T: 10600 FC
OR
72100 FH
*
*
*
*
*
FC OPTIMIZED:
T: 11100 FC
OR
36300 FH
TBD
TBD
TBD
TBD
TBD
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 136
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
533127-03-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
* * * * *
C O N T I N U E
SOURCE
REFERENCE
MEN
M/H
APPLICABILITY
* * * * *
I: 11100 FC
OR
36300 FH
533127-03-2
191
192
193
195
196
AIR CONDITIONING ACCESS CUTOUT
AF
DET
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
FH OPTIMIZED:
T: 7600 FC
OR
49700 FH
I:
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
PANELS
PANELS
PANELS
PANELS
PANELS
Z191;
Z192;
Z193;
Z195;
Z196;
191
192
193
195
196
AIR CONDITIONING ACCESS CUTOUT
AF
DET
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
PANELS
PANELS
PANELS
PANELS
PANELS
Z191;
Z192;
Z193;
Z195;
Z196;
1
1
1
1
1
*
*
*
*
*
0.10 GROUP 32A
0.10
0.10
0.10
0.10
TBD
TBD
TBD
TBD
TBD
8100 FC
OR
26600 FH
ALI
533100-220-801
ALI REFERENCE:
533127-03-03
6500 FC
OR
42900 FH
1
1
1
1
1
*
*
*
*
*
FC OPTIMIZED:
T: 6800 FC
OR
22400 FH
I:
STRUCTURE : FUSELAGE
ALI REFERENCE:
533127-03-02
7600 FC
OR
49700 FH
FH OPTIMIZED:
T: 6500 FC
OR
42900 FH
I:
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
533100-220-801
FC OPTIMIZED:
T: 8100 FC
OR
26600 FH
I:
533127-03-3
ALI
0.10 GROUP 32E
0.10 OR
0.10 GROUP 33E
0.10
0.10
TBD
TBD
TBD
TBD
TBD
6800 FC
OR
22400 FH
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 137
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533127-03-4
ZONE
191
192
193
195
196
AIR CONDITIONING ACCESS CUTOUT
191
192
193
195
196
AF
DET
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
533127-03-5
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
PANELS
PANELS
PANELS
PANELS
PANELS
T: 19000 FC
I: 19000 FC
AF
DET
FH OPTIMIZED:
T: 8600 FC
OR
58700 FH
I:
533127-03-6
191
192
193
195
196
Z191;
Z192;
Z193;
Z195;
Z196;
AIR CONDITIONING ACCESS CUTOUT
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
PANELS
PANELS
PANELS
PANELS
PANELS
ALI REFERENCE:
533127-03-04
1
1
1
1
1
ALI
533100-220-801
ALI REFERENCE:
533127-03-05
8600 FC
OR
58700 FH
1
1
1
1
1
*
M/H
APPLICABILITY
0.10 A330-200F
0.10
0.10
0.10
0.10
TBD
TBD
TBD
TBD
TBD
0.10 GROUP 33C
0.10 OR
0.10 GROUP 33D
0.10
0.10
TBD
FC OPTIMIZED:
T: 9000 FC
OR
29500 FH
AF
DET
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
STRUCTURE : FUSELAGE
PANELS
PANELS
PANELS
PANELS
PANELS
533100-220-801
MEN
*
*
*
*
*
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
ALI
REFERENCE
Z191;
Z192;
Z193;
Z195;
Z196;
AIR CONDITIONING ACCESS CUTOUT
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
SOURCE
I:
9000 FC
OR
29500 FH
T:
6000 FC
I:
6000 FC
ALI
533100-220-801
ALI REFERENCE:
533127-03-06
Z191;
Z192;
Z193;
Z195;
Z196;
1
1
1
1
1
*
REV. DATE: JUL 01/21
SECTION:
3-53
0.10 A330-900
0.10
0.10
0.10
0.10
TBD
PAGE 138
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
N
533127-03-7
ZONE
191
192
193
195
196
AIR CONDITIONING ACCESS CUTOUT
143
149
191
192
193
195
196
FAIRING
FAIRING
FAIRING
FAIRING
FAIRING
MAIN STRUCTURE
DET
PANELS
PANELS
PANELS
PANELS
PANELS
T:
8200 FC
I:
8200 FC
T:
12 YE
DETAILED INSPECTION OF KEEL BEAM INTERNAL AND
EXTERNAL STRUCTURE SKIN AND ADJACENT FUSELAGE
STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE.
I:
12 YE
TPS
SOURCE
ALI
REFERENCE
533100-220-801
ALI REFERENCE:
533127-03-07
Z191;
Z192;
Z193;
Z195;
Z196;
DET
AF
MRB CPCP
533100-220-804
MRB REFERENCE:
533129-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
191KB
193BB
195CB
533135-01-1
AF
DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING
ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)
EXTERNAL SURFACE.
PREP.: BELLY
BELLY
BELLY
BELLY
BELLY
533129-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
193DB
195DB
147 MAIN STRUCTURE
AF
DET
148
149 DETAILED INSPECTION OF CENTER LANDING GEAR AND MAIN
LANDING GEAR DOOR HINGE FITTINGS 1 THROUGH 6, DOOR
ACTUATOR FITTINGS AND THEIR ATTACHMENT TO THE KEEL
BEAM, LH/RH.
T:
12 YE
I:
12 YE
MRB CPCP
533100-200-813
MRB REFERENCE:
533135-01-1
MEN
M/H
APPLICABILITY
1
1
1
1
1
TBD A330-800
TBD
TBD
TBD
TBD
*
TBD
1
1
1
1
1
1
1
0.15 ALL
0.15
0.15
0.15
0.15
0.15
0.15
*
*
*
*
*
0.15
0.15
2.00
3.50
3.50
1
1
1
0.50 ALL
0.50
0.50
*
*
0.15
0.15
(A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE
A330. HOWEVER, THE TERM CENTER LANDING GEAR HAS BEEN
KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL
COMMONALITY WITH THE A340 IN THIS AREA.)
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 734
744
STRUCTURE : FUSELAGE
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 139
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533138-01-2
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
145 MAIN STRUCTURE
NDT SDI
146
SPECIAL DETAILED INSPECTION (X-RAY) OF FUSELAGE
INTERNAL STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y=
1959 AT FR 48 LEVEL, LH/RH.
FH OPTIMIZED:
T: 14500 FC
OR
98200 FH
I:
NOTE:
FOR AIRCRAFT POST 42418 THRESHOLD IS TO BE COUNTED
FROM SB 53-3013 EMBODIMENT.
151 MAIN STRUCTURE
AF
DET
152
DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND
PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND
CARGO COMPARTMENT FLOOR LEVEL.
TPS
ALI
REFERENCE
533100-260-812
I:
8900 FC
OR
26900 FH
T:
12 YE
I:
12 YE
*
MRB CPCP
533100-200-814
MRB REFERENCE:
533141-01-1
151BW
152CW
151CW
822
137 MAIN STRUCTURE
AF
DET
138
DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER
WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE
INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE AND
STR 40, FROM AFT FACE OF CARGO COMPARTMENT REAR PANEL
TO FR 40.
T:
12 YE
I:
12 YE
MRB CPCP
533100-200-815
1.50 GROUP 33A
1.50 POST 42418 S11867
OR
GROUP 33A
POST SB 53-3013
>99.9
1
1
0.75 ALL
0.75
*
0.01
*
*
0.55
0.30
1
1
0.75 ALL
0.75
*
1.00
MRB REFERENCE:
533142-01-1
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: AIR CONDITIONING DUCTS Z137/Z138;
* * * * *
STRUCTURE : FUSELAGE
APPLICABILITY
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
ACCESS: 151AW
152BW
TPS
2
2
M/H
7100 FC
OR
48500 FH
PREP.: LDL (IF INSTALLED);
LDMCR (IF INSTALLED);
533142-01-1
MEN
ALI REFERENCE:
533138-01-02
FC OPTIMIZED:
T: 18100 FC
OR
54500 FH
PREP.: FLOOR PANELS Z250;
INSULATION Z250;
533141-01-1
SOURCE
C O N T I N U E D
* * * * *
REV. DATE: JUL 01/21
SECTION:
3-53
PAGE 140
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
533142-01-1
* * * * *
ACCESS: 131BX
132CX
533143-01-1
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
C O N T I N U E
131CX
132DX
131DX
REFERENCE
821
DET
T:
6 YE
I:
6 YE
MRB CPCP
533100-220-802
M/H
*
*
0.55
0.30
1
1
0.30 ALL
0.30
APPLICABILITY
MRB REFERENCE:
533143-01-1
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
PREP.: FLOOR PANELS Z150;
LDL (IF INSTALLED);
LDMCR (IF INSTALLED);
533144-01-1
MEN
* * * * *
153 MAIN STRUCTURE
AF
154
DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND
PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR
LEVEL.
TPS
SOURCE
*
137 MAIN STRUCTURE
AF
DET
138
DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER
WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE
INTERNAL STRUCTURE BELOW STR 40, FROM FR 39.1 TO FR
40.
T:
6 YE
I:
6 YE
MRB CPCP
533100-220-803
19.01
1
1
0.30 ALL
0.30
PREP.: AIR CONDITIONING DUCTS Z137/Z138;
*
1.00
ACCESS: 131BX
132CX
*
*
0.40
0.15
1
1
0.20 GROUP 32A
0.20 PRE 49202
MRB REFERENCE:
533144-01-1
NOTE:
APPLY AFTER INSPECTION IN ADDITION TO TYPE 1 TYPE 2
TEMPORARY PROTECTION SYSTEM ON FWD FACE OF FR 40 AND
ON FUSELAGE STRUCTURE FROM 25 CM AFTER FR 39.2 TO FR
40.
TPS
533145-01-4
: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT,
APPLICATION OF TPS TYPE 2
821
100 MAIN STRUCTURE
197
* * * * *
STRUCTURE : FUSELAGE
131CX
NDT
C O N T I N U E D
SDI
T: 32600 FC
ALI WFD
533100-200-844
* * * * *
REV. DATE: JUL 01/21
SECTION:
3 -53
PAGE 141
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
533145-01-4
* * * * *
C O N T I N U E
533145-01-5
533150-01-1
I:
7300 FC
ALI REFERENCE:
533145-01-04
197HB
198HB
MEN
T: 42300 FC
I:
ALI WFD
8300 FC
533100-200-844
ALI REFERENCE:
533145-01-03
197HB
198HB
145 MAIN STRUCTURE
AF
146
DETAILED INSPECTION OF PRESSURIZED FLOORS AND
PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL
FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.
1
*
*
100 MAIN STRUCTURE
NDT SDI
197
198 SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
LONGITUDINAL BUTT JOINT AT STR 31 LEVEL FROM FR 53.3
TO FR 54, LH/RH.
ACCESS: 197AT
198AT
REFERENCE
DET
T:
6 YE
I:
6 YE
MRB CPCP
533100-200-819
MRB REFERENCE:
533150-01-1
*
*
4.20
4.20
1
1
1.00 A330-200
1.00 GALLEYS/ TOILETS
INSTALLED BETWEEN
FR 47 AND FR 53.2,
SEE NOTE
OR
A330-300
GALLEYS/ TOILETS
INSTALLED BETWEEN
FR 47 AND FR 53.2,
SEE NOTE
OR
7.00 A330-800
GALLEYS/ TOILETS
INSTALLED BETWEEN
FR 47 AND FR 53.2,
SEE NOTE
OR
A330-900
GALLEYS/ TOILETS
INSTALLED BETWEEN
FR 47 AND FR 53.2,
SEE NOTE
*
REV. DATE: JUL 01/21
SECTION:
3-53
0.20 OR
GROUP 33B
OR
GROUP 33C
4.20 PRE 49202
4.20 OR
GROUP 33D
PRE 49202
0.20 GROUP 33A
0.20
0.20
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: CABIN FLOOR PANELS Z250;
GALLEYS Z250;
LAVATORIES Z250;
STRUCTURE : FUSELAGE
APPLICABILITY
1
1
1
NOTE:
TASK APPLICABLE IF GALLEYS OR TOILETS ARE FITTED
ABOVE THIS AREA.
TPS
M/H
* * * * *
198 SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE
LONGITUDINAL BUTT JOINT AT STR 31 LEVEL FROM FR 53.3
TO FR 54, LH/RH.
ACCESS: 197AT
198AT
SOURCE
PAGE 142
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533150-02-1
ZONE
SAMPLE THRESHOLD (ST)
SAMPLE INTERVAL (SI)
THRESHOLD (T)
INTERVAL (I)
DESCRIPTION
145 MAIN STRUCTURE
AF
146
DETAILED INSPECTION OF PRESSURIZED FLOORS AND
PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL
FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.
DET
T:
12 YE
I:
12 YE
SOURCE
MRB CPCP
REFERENCE
533100-200-836
MEN
1
1
MRB REFERENCE:
533150-01-2
M/H
APPLICABILITY
1.00 IF GALLEYS/ TOILETS
1.00 NOT INSTALLED
BETWEEN FR 47 AND
FR 53.2, SEE NOTE
NOTE:
- TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT
FITTED ABOVE THIS AREA.
- TPS APPLICATION MAY BE LIMITED TO PRESSURIZED
FLOORS AND PRESSURE DIAPHRAGM.
TPS
: APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3
PREP.: CABIN FLOOR PANELS Z250;
533152-01-2
STRUCTURE : FUSELAGE
151 MAIN STRUCTURE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF STR 31, INTERNAL
FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET
FAIRING LEVEL, LH/RH.
*
T: 32600 FC
I:
ALI WFD
7300 FC
533100-270-811
1
1
ALI REFERENCE:
533152-01-04
PREP.: ACT IF INSTALLED;
*
ACCESS: 151GW
152GW
*
*
REV. DATE: JUL 01/21
SECTION:
3 -53
TBD
0.75 GROUP 32A
0.75 PRE 40379
(25-3168),
(25-3363)
PRE 46202
PRE 49202
TBD OR
GROUP 33B
0.20 PRE 40379
0.20 (25-3168),
(25-3363)
PRE 46202
OR
GROUP 33C
PRE 40161
PRE 40379
(25-3168),
(25-3363)
PRE 46202
PRE 49202
OR
GROUP 33D
PRE 40379
(25-3168),
(25-3363)
PRE 46202
PRE 49202
PAGE 143
MAINTENANCE PLANNING DOCUMENT
HEADERLI NE
TASK NUMBER
533152-01-3
533152-01-4
533152-02-2
ZONE
151 MAIN STRUCTURE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF STR 31, INTERNAL
FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET
FAIRING LEVEL, LH/RH.
APPLICABILITY
*
*
0.20
0.20
1
1
0.75 GROUP 33A
0.75 PRE 40379
(25-3168),
(25-3363)
PRE 46202
T: 42300 FC
I:
1
1
M/H
ACCESS: 151GW
152GW
7300 FC
533100-270-811
MEN
*
I:
ALI WFD
REFERENCE
PREP.: ACT IF INSTALLED;
151 MAIN STRUCTURE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF STR 31, INTERNAL
FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET
FAIRING LEVEL, LH/RH.
T: 40000 FC
SOURCE
0.75 GROUP 33C
0.75 POST 40161
PRE 40379
(25-3168),
(25-3363)
PRE 46202
TBD PRE 49202
ALI REFERENCE:
533152-01-07
ALI WFD
8300 FC
533100-270-811
ALI REFERENCE:
533152-01-01
PREP.: ACT IF INSTALLED;
*
TBD
ACCESS: 151GW
152GW
*
*
0.20
0.20
1
1
0.75 GROUP 32A
0.75 POST 40379
(25-3168),
(25-3363)
PRE 46202
PRE 49202
TBD OR
GROUP 33B
POST 40379
0.20 (25-3168),
0.15 (25-3363)
PRE 46202
OR
GROUP 33C
PRE 40161
POST 40379
(25-3168),
(25-3363)
PRE 46202
PRE 49202
OR
151 MAIN STRUCTURE
NDT SDI
152
SPECIAL DETAILED INSPECTION (US) OF STR 31, INTERNAL
FUSELAGE, BETWEEN FR 53.7 AND F